Hybrid band intelligent backhaul radio

ABSTRACT

A hybrid band intelligent backhaul radio (HB-IBR) is disclosed that is a combination of two radios operating in different bands. Embodiments include a dual radio configuration wherein a first radio operates in a non-line of sight (NLOS) radio link configuration and a second ancillary radio operates in a near line of sight or line of sight configuration (n)LOS. For example, the HB-IBR may have an Intelligent Backhaul Radio (IBR) operating in the non-line of sight mode of operation within the 5.8 GHz unlicensed band, and have an ancillary radio link operating in the FCC part 101 E band of operation at 60 GHz. A common medium access control (MAC) block may be utilized between the dual radios.

CROSS-REFERENCE TO RELATED APPLICATION

The present application is a continuation application of U.S. patentapplication Ser. No. 13/448,294, filed on Apr. 16, 2012, and thedisclosure of which is hereby incorporated herein by reference in itsentirety.

BACKGROUND

1. Field

The present disclosure relates generally to data networking and inparticular to a backhaul radio for connecting remote edge accessnetworks to core networks. In some embodiments, the present disclosurerelates to the use of multiple radio links operating within differentbands between common backhaul radio installations.

2. Related Art

Data networking traffic has grown at approximately 100% per year forover 20 years and continues to grow at this pace. Only transport overoptical fiber has shown the ability to keep pace with thisever-increasing data networking demand for core data networks. Whiledeployment of optical fiber to an edge of the core data network would beadvantageous from a network performance perspective, it is oftenimpractical to connect all high bandwidth data networking points withoptical fiber at all times. Instead, connections to remote edge accessnetworks from core networks are often achieved with wireless radio,wireless infrared, and/or copper wireline technologies.

Radio, especially in the form of cellular or wireless local area network(WLAN) technologies, is particularly advantageous for supportingmobility of data networking devices. However, cellular base stations orWLAN access points inevitably become very high data bandwidth demandpoints that require continuous connectivity to an optical fiber corenetwork.

When data aggregation points, such as cellular base station sites, WLANaccess points, or other local area network (LAN) gateways, cannot bedirectly connected to a core optical fiber network, then an alternativeconnection, using, for example, wireless radio or copper wirelinetechnologies, must be used. Such connections are commonly referred to as“backhaul.”

Many cellular base stations deployed to date have used copper wirelinebackhaul technologies such as T1, E1, DSL, etc. when optical fiber isnot available at a given site. However, the recent generations of HSPA+and LTE cellular base stations have backhaul requirements of 100 Mb/s ormore, especially when multiple sectors and/or multiple mobile networkoperators per cell site are considered. WLAN access points commonly havesimilar data backhaul requirements. These backhaul requirements cannotbe practically satisfied at ranges of 300 m or more by existing copperwireline technologies. Even if LAN technologies such as Ethernet overmultiple dedicated twisted pair wiring or hybrid fiber/coax technologiessuch as cable modems are considered, it is impractical to backhaul atsuch data rates at these ranges (or at least without adding intermediaterepeater equipment). Moreover, to the extent that such special wiring(i.e., CAT 5/6 or coax) is not presently available at a remote edgeaccess network location; a new high capacity optical fiber isadvantageously installed instead of a new copper connection.

Rather than incur the large initial expense and time delay associatedwith bringing optical fiber to every new location, it has been common tobackhaul cell sites, WLAN hotspots, or LAN gateways from offices,campuses, etc. using microwave radios. An exemplary backhaul connectionusing the microwave radios 132 is shown in FIG. 1. Traditionally, suchmicrowave radios 132 for backhaul have been mounted on high towers 112(or high rooftops of multi-story buildings) as shown in FIG. 1, suchthat each microwave radio 132 has an unobstructed line of sight (LOS)136 to the other. These microwave radios 132 can have data rates of 100Mb/s or higher at unobstructed LOS ranges of 300 m or longer withlatencies of 5 ms or less (to minimize overall network latency).

Traditional microwave backhaul radios 132 operate in a Point to Point(PTP) configuration using a single “high gain” (typically >30 dBi oreven >40 dBi) antenna at each end of the link 136, such as, for example,antennas constructed using a parabolic dish. Such high gain antennasmitigate the effects of unwanted multipath self-interference or unwantedco-channel interference from other radio systems such that high datarates, long range and low latency can be achieved. These high gainantennas however have narrow radiation patterns.

Furthermore, high gain antennas in traditional microwave backhaul radios132 require very precise, and usually manual, physical alignment oftheir narrow radiation patterns in order to achieve such highperformance results. Such alignment is almost impossible to maintainover extended periods of time unless the two radios have a clearunobstructed line of sight (LOS) between them over the entire range ofseparation. Furthermore, such precise alignment makes it impractical forany one such microwave backhaul radio to communicate effectively withmultiple other radios simultaneously (i.e., a “point to multipoint”(PMP) configuration).

In wireless edge access applications, such as cellular or WLAN, advancedprotocols, modulation, encoding and spatial processing across multipleradio antennas have enabled increased data rates and ranges for numeroussimultaneous users compared to analogous systems deployed 5 or 10 yearsago for obstructed LOS propagation environments where multipath andco-channel interference were present. In such systems, “low gain”(usually <6 dBi) antennas are generally used at one or both ends of theradio link both to advantageously exploit multipath signals in theobstructed LOS environment and allow operation in different physicalorientations as would be encountered with mobile devices. Althoughimpressive performance results have been achieved for edge access, suchresults are generally inadequate for emerging backhaul requirements ofdata rates of 100 Mb/s or higher, ranges of 300 m or longer inobstructed LOS conditions, and latencies of 5 ms or less.

In particular, “street level” deployment of cellular base stations, WLANaccess points or LAN gateways (e.g., deployment at street lamps, trafficlights, sides or rooftops of single or low-multiple story buildings)suffers from problems because there are significant obstructions for LOSin urban environments (e.g., tall buildings, or any environments wheretall trees or uneven topography are present).

FIG. 1 illustrates edge access using conventional unobstructed LOS PTPmicrowave radios 132. The scenario depicted in FIG. 1 is common for many2^(nd) Generation (2G) and 3^(rd) Generation (3G) cellular networkdeployments using “macrocells”. In FIG. 1, a Cellular Base TransceiverStation (BTS) 104 is shown housed within a small building 108 adjacentto a large tower 112. The cellular antennas 116 that communicate withvarious cellular subscriber devices 120 are mounted on the towers 112.The PTP microwave radios 132 are mounted on the towers 112 and areconnected to the BTSs 104 via an nT1 interface. As shown in FIG. 1 byline 136, the radios 132 require unobstructed LOS.

The BTS on the right 104 a has either an nT1 copper interface or anoptical fiber interface 124 to connect the BTS 104 a to the Base StationController (BSC) 128. The BSC 128 either is part of or communicates withthe core network of the cellular network operator. The BTS on the left104 b is identical to the BTS on the right 104 a in FIG. 1 except thatthe BTS on the left 104 b has no local wireline nT1 (or optical fiberequivalent) so the nT1 interface is instead connected to a conventionalPTP microwave radio 132 with unobstructed LOS to the tower on the right112 a. The nT1 interfaces for both BTSs 104 a, 104 b can then bebackhauled to the BSC 128 as shown in FIG. 1.

FIG. 2 is a block diagram of the major subsystems of a conventional PTPmicrowave radio 200 for the case of Time-Division Duplex (TDD)operation, and FIG. 3 is a block diagram of the major subsystems of aconventional PTP microwave radio 300 for the case of Frequency-DivisionDuplex (FDD) operation.

As shown in FIG. 2 and FIG. 3, the conventional PTP microwave radiotraditionally uses one or more (i.e. up to “n”) T1 interfaces 204 (or inEurope, E1 interfaces). These interfaces 204 are common in remote accesssystems such as 2G cellular base stations or enterprise voice and/ordata switches or edge routers. The T1 interfaces are typicallymultiplexed and buffered in a bridge (e.g., the Interface Bridge 208,308) that interfaces with a Media Access Controller (MAC) 212, 312.

The MAC 212, 312 is generally denoted as such in reference to asub-layer of Layer 2 within the Open Systems Interconnect (OSI)reference model. Major functions performed by the MAC include theframing, scheduling, prioritizing (or “classifying”), encrypting anderror checking of data sent from one such radio at FIG. 2 or FIG. 3 toanother such radio. The data sent from one radio to another is generallyin a “user plane” if it originates at the T1 interface(s) or in the“control plane” if it originates internally such as from the Radio LinkController (RLC) 248, 348 shown in FIG. 2 or FIG. 3. A typical MAC frameformat 400 (known as a MAC protocol data unit, or “MPDU”) with header404, frame body 408 and frame check sum (FCS) 412 is shown in FIG. 4.

With reference to FIGS. 2 and 3, the Modem 216, 316 typically resideswithin the “baseband” portion of the Physical (PHY) layer 1 of the OSIreference model. In conventional PTP radios, the baseband PHY, depictedby Modem 216, 316, typically implements scrambling, forward errorcorrection encoding, and modulation mapping for a single RF carrier inthe transmit path. In receive, the modem typically performs the inverseoperations of demodulation mapping, decoding and descrambling. Themodulation mapping is conventionally Quadrature Amplitude Modulation(QAM) implemented with In-phase (I) and Quadrature-phase (Q) branches.

The Radio Frequency (RF) 220, 320 also resides within the PHY layer ofthe radio. In conventional PTP radios, the RF 220, 320 typicallyincludes a single transmit chain (Tx) 224, 324 that includes I and Qdigital to analog converters (DACs), a vector modulator, optionalupconverters, a programmable gain amplifier, one or more channelfilters, and one or more combinations of a local oscillator (LO) and afrequency synthesizer. Similarly, the RF 220, 320 also typicallyincludes a single receive chain (Rx) 228, 328 that includes I and Qanalog to digital converters (ADCs), one or more combinations of an LOand a frequency synthesizer, one or more channel filters, optionaldownconverters, a vector demodulator and an automatic gain control (AGC)amplifier. Note that in many cases some of the one or more LO andfrequency synthesizer combinations can be shared between the Tx and Rxchains.

As shown in FIGS. 2 and 3, conventional PTP radios 200, 300 also includea single power amplifier (PA) 232, 332. The PA 232, 332 boosts thetransmit signal to a level appropriate for radiation from the antenna inkeeping with relevant regulatory restrictions and instantaneous linkconditions. Similarly, such conventional PTP radios 232, 332 typicallyalso include a single low-noise amplifier (LNA) 236, 336 as shown inFIGS. 2 and 3. The LNA 236, 336 boosts the received signal at theantenna while minimizing the effects of noise generated within theentire signal path.

As described above, FIG. 2 illustrates a conventional PTP radio 200 forthe case of TDD operation. As shown in FIG. 2, conventional PTP radios200 typically connect the antenna 240 to the PA 232 and LNA 236 via aband-select filter 244 and a single-pole, single-throw (SPST) switch242.

As described above, FIG. 3 illustrates a conventional PTP radio 300 forthe case of FDD operation. As shown in FIG. 3, in conventional PTPradios 300, then antenna 340 is typically connected to the PA 332 andLNA 336 via a duplexer filter 344. The duplexer filter 344 isessentially two band-select filters (tuned respectively to the Tx and Rxbands) connected at a common point.

In the conventional PTP radios shown in FIGS. 2 and 3, the antenna 240,340 is typically of very high gain such as can be achieved by aparabolic dish so that gains of typically >30 dBi (or even sometimes >40dBi), can be realized. Such an antenna usually has a narrow radiationpattern in both the elevation and azimuth directions. The use of such ahighly directive antenna in a conventional PTP radio link withunobstructed LOS propagation conditions ensures that the modem 216, 316has insignificant impairments at the receiver (antenna 240, 340) due tomultipath self-interference and further substantially reduces thelikelihood of unwanted co-channel interference due to other nearby radiolinks.

Although not explicitly shown in FIGS. 2 and 3, the conventional PTPradio may use a single antenna structure with dual antenna feedsarranged such that the two electromagnetic radiation patterns emanatedby such an antenna are nominally orthogonal to each other. An example ofthis arrangement is a parabolic dish. Such an arrangement is usuallycalled dual-polarized and can be achieved either by orthogonal verticaland horizontal polarizations or orthogonal left-hand circular andright-hand circular polarizations.

When duplicate modem blocks, RF blocks, and PA/LNA/switch blocks areprovided in a conventional PTP radio, then connecting each PHY chain toa respective polarization feed of the antenna allows theoretically up totwice the total amount of information to be communicated within a givenchannel bandwidth to the extent that cross-polarizationself-interference can be minimized or cancelled sufficiently. Such asystem is said to employ “dual-polarization” signaling.

When an additional circuit (not shown) is added to FIG. 2 that canprovide either the RF Tx signal or its anti-phase equivalent to eitherone or both of the two polarization feeds of such an antenna, then“cross-polarization” signaling can be used to effectively expand theconstellation of the modem within any given symbol rate or channelbandwidth. With two polarizations and the choice of RF signal or itsanti-phase, then an additional two information bits per symbol can becommunicated across the link. Theoretically, this can be extended andexpanded to additional phases, representing additional information bits.At the receiver, for example, a circuit (not shown) could detect if thetwo received polarizations are anti-phase with respect to each other, ornot, and then combine appropriately such that the demodulator in themodem block can determine the absolute phase and hence deduce the valuesof the two additional information bits. Cross-polarization signaling hasthe advantage over dual-polarization signaling in that it is generallyless sensitive to cross-polarization self-interference but for highorder constellations such as 64-QAM or 256-QAM, the relative increase inchannel efficiency is smaller.

In the conventional PTP radios shown in FIGS. 2 and 3, substantially allthe components are in use at all times when the radio link is operative.However, many of these components have programmable parameters that canbe controlled dynamically during link operation to optimize throughoutand reliability for a given set of potentially changing operatingconditions. The conventional PTP radios of FIGS. 2 and 3 control theselink parameters via a Radio Link Controller (RLC) 248, 348. The RLCfunctionality is also often described as a Link Adaptation Layer that istypically implemented as a software routine executed on amicrocontroller within the radio that can access the MAC 212, 312, Modem216, 316, RF 220, 320 and/or possibly other components with controllableparameters. The RLC 248, 348 typically can both vary parameters locallywithin its radio and communicate with a peer RLC at the other end of theconventional PTP radio link via “control frames” sent by the MAC 212,312 with an appropriate identifying field within a MAC Header 404 (inreference to FIG. 4).

Typical parameters controllable by the RLC 248, 348 for the Modem 216,316 of a conventional PTP radio include encoder type, encoding rate,constellation selection and reference symbol scheduling and proportionof any given PHY Protocol Data Unit (PPDU). Typical parameterscontrollable by the RLC 248, 348 for the RF 220, 320 of a conventionalPTP radio include channel frequency, channel bandwidth, and output powerlevel. To the extent that a conventional PTP radio employs twopolarization feeds within its single antenna, additional parameters mayalso be controlled by the RLC 248, 348 as self-evident from thedescription above.

In conventional PTP radios, the RLC 248, 348 decides, usuallyautonomously, to attempt such parameter changes for the link in responseto changing propagation environment characteristics such as, forexample, humidity, rain, snow, or co-channel interference. There areseveral well-known methods for determining that changes in thepropagation environment have occurred such as monitoring the receivesignal strength indicator (RSSI), the number of or relative rate of FCSfailures at the MAC 212, 312, and/or the relative value of certaindecoder accuracy metrics. When the RLC 248, 348 determines thatparameter changes should be attempted, it is necessary in most casesthat any changes at the transmitter end of the link become known to thereceiver end of the link in advance of any such changes. Forconventional PTP radios, and similarly for many other radios, there areat least two well-known techniques which in practice may not be mutuallyexclusive. First, the RLC 248, 348 may direct the PHY, usually in theModem 216, 316 relative to FIGS. 2 and 3, to pre-pend a PHY layerconvergence protocol (PLCP) header to a given PPDU that includes one ormore (or a fragment thereof) given MPDUs wherein such PLCP header hasinformation fields that notify the receiving end of the link ofparameters used at the transmitting end of the link. Second, the RLC248, 348 may direct the MAC 212, 312 to send a control frame, usually toa peer RLC 248, 348, including various information fields that denotethe link adaptation parameters either to be deployed or to be requestedor considered.

One particularly interesting band for which significant spectrum isgenerally available is the so called “E Band”, which operates at themillimeter wave band (70 GHz to 90 GHz). Due to the high frequencies ofoperation, relatively higher channel bandwidths are available.

The L Band, used by the conventional PTP radios, allows for the use ofwide RF channels (e.g., 250 MHz to 500 MHz). Such wide bandwidthchannels allow very high modulation rates for radios utilizing thisspectrum, resulting in a data link which may exceed 1 GBPSbidirectional.

A property of the E Band, due to its millimeter wave frequencyallocation, is a higher radio frequency propagation loss. Thispropagation loss has the benefit of reducing the opportunity for theproblem of interference to or from other stations operating on the samefrequency channels. One disadvantage of the increased signal propagationloss is that signals between two stations in a point to point radio linkdo not propagate as far, resulting in reduced link range. Typically,point to point radio links operating within the E Band compensate forthe increased signal propagation loss by utilizing high gain antennas.The high gain antennas allow for an increase in the operating range ofthe point to point link. A fundamental property of antennas is that toincrease the gain of the antenna, the directivity must be increased anda resulting antenna beam width proportionally deduced. To achieve thedesired practical links gains, typical E band antennas have an antennabeam width of 0.5 degrees. Such narrow beam widths result in asignificantly reduced probability of interference from or to otherco-channel E Band links. The combination of increased propagation loss,and reduced antenna beam widths allow for a simpler and FCC licenseapproval under 47 Code of Federal Regulations (C.F.R.) §101.

However, as previously described, the use of high gain antennas requiresprecise alignment of the antenna peak gain. The antenna alignment neededfor point to point L band operation requires multiple skilledtechnicians to perform a precise alignment process at each end of thelink. This alignment process is often dependent on the skill of thespecific technicians and can result in variable results and linkperformance. Exemplary variations that can affect the results and linkperformance in temperature variation, structure vibration, ageing ofcomponents, and other variations. In some installations, the techniciansmay align the antennas for “sufficiency” rather than optimality. As aresult, the link may be configured with parameters “on the edge” ofoperation, which may result in failure of the link at future points intime. The metrics used for determining alignment are generally receivedtransmission power from one radio to the other, which may be simplisticrelative to performance of the link. The current installations do nothave the ability to “self-heal” or adapt to changing structure orvarying operating conditions, resulting in a potential lack ofrobustness in the link operation and performance.

The foregoing describes at an overview level the typical structural andoperational features of conventional PTP radios which have been deployedin real-world conditions for many radio links where unobstructed (orsubstantially unobstructed) LOS propagation was possible. Theconventional PTP radio on a whole is completely unsuitable forobstructed LOS or PMP operation.

SUMMARY

The following summary of the invention is included in order to provide abasic understanding of some aspects and features of the invention. Thissummary is not an extensive overview of the invention and as such it isnot intended to particularly identify key or critical elements of theinvention or to delineate the scope of the invention. Its sole purposeis to present some concepts of the invention in a simplified form as aprelude to the more detailed description that is presented below.

Some embodiments of the claimed invention are directed to backhaulradios that are compact, light and low power for street level mounting,operate at 100 Mb/s or higher at ranges of 300 m or longer in obstructedLOS conditions with low latencies of 5 ms or less, can support PTP andPMP topologies, use radio spectrum resources efficiently and do notrequire precise physical antenna alignment. Radios with such exemplarycapabilities as described by multiple various embodiments are referredto herein by the term “Intelligent Backhaul Radio” (IBR).

According to an aspect of the invention, an intelligent backhaul radiois disclosed that includes one or more demodulator cores, wherein eachdemodulator core demodulates one or more receive symbol streams toproduce a respective receive data interface stream; a plurality ofreceive RF chains to convert from a plurality of receive RF signals to aplurality of respective receive chain output signals; a frequencyselective receive path channel multiplexer, interposed between the oneor more demodulator cores and the plurality of receive RF chains, toproduce the one or more receive symbol streams provided to the one ormore demodulator cores from the plurality of receive chain outputsignals; an antenna array including: a plurality of directive gainantenna elements; and one or more selectable RF connections thatselectively couple certain of the plurality of directive gain antennaelements to certain of the plurality of receive RF chains, wherein thenumber of directive gain antenna elements that can be selectivelycoupled to receive RF chains exceeds the number of receive RF chainsthat can accept receive RF signals from the one or more selectable RFconnections; and a radio resource controller, wherein the radio resourcecontroller sets or causes to be set the specific selective couplingsbetween the certain of the plurality of directive gain antenna elementsand the certain of the plurality of receive RF chains.

At least two or more of the directive gain antenna elements that can beselectively coupled to receive RF chains may be oriented in differentdirections to provide directional diversity.

The set of directive gain antenna elements that can be selectivelycoupled to receive RF chains may include directive gain antenna elementsof at least two different orthogonal polarizations.

The set of the directive gain antenna elements that can be selectivelycoupled to receive RF chains may be divided between one subset with afirst polarization and a second subset with a second polarization. Thefirst polarization may be vertical and the second polarization may behorizontal. The first polarization may be left-hand circular and thesecond polarization may be right-hand circular.

The set of receive RF chains that can accept receive RF signals from theone or more selectable RF connections may be divided between one subsetthat accepts receive RF signals from directive gain antenna elementswith the first polarization and a second subset that accepts receive RFsignals from directive gain antenna elements with a second polarization.

The directive gain antenna elements that can be selectively coupled toreceive RF chains may be arranged on a plurality of facets with one ormore directive gain antenna elements per facet, and each facet may beoriented at a different angle in the azimuth relative to at least oneother facet.

The one or more selectable RF connections may be arranged such that anyreceive RF chains that can accept receive RF signals from the one ormore selectable RF connections can be selectively coupled to directivegain antenna elements from more than one facet.

The one or more selectable RF connections may be arranged such that theset of receive RF chains that can accept receive RF signals from the oneor more selectable RF connections can be selectively coupled todirective gain antenna elements from any two facets sharing a commonprojected edge.

The one or more selectable RF connections may be arranged such the setof receive RF chains that can accept receive RF signals from the one ormore selectable RF connections can be selectively coupled to directivegain antenna elements from any two facets closest to each other inazimuthal angle amongst all facets include directive gain antennaelements that can be selectively coupled to receive RF chains.

Each facet may include directive gain antenna elements of at least twodifferent orthogonal polarizations.

One or more directive gain antenna elements or other antenna elementswithin the antenna array may be coupled to one or more respectivereceive RF chains other than by said one or more selectable RFconnections.

The one or more respective receive RF chains may be coupled to the oneor more directive gain antenna elements or other antenna elements withinthe antenna array other than by said one or more selectable RFconnections may be each coupled to a respective Discrete FourierTransformer within the frequency selective receive path channelmultiplexer.

The intelligent backhaul radio may further include one or more modulatorcores, wherein each modulator core modulates a respective transmit datainterface stream to produce one or more transmit symbol streams; aplurality of transmit RF chains to convert from a plurality of transmitchain input signals to a plurality of respective transmit RF signals; atransmit path channel multiplexer, interposed between the one or moremodulator cores and the plurality of transmit RF chains, to produce theplurality of transmit chain input signals provided to the plurality oftransmit RF chains from the one or more transmit symbol streams; and,wherein the antenna array further includes a plurality of RF connectionsto couple at least certain of the plurality of directive gain antennaelements to the plurality of transmit RF chains.

The number of transmit RF chains may equal the number of transmit symbolstreams.

The transmit path channel multiplexer may couple the plurality oftransmit RF chains to respective transmit symbol streams such that eachrespective transmit chain input signal includes information from onlyone respective transmit symbol stream.

The number of transmit RF chains may exceed the number of transmitsymbol streams, and the transmit path channel multiplexer may couple atleast one set of two or more of the plurality of transmit RF chains to aparticular transmit symbol stream such that each transmit chain inputsignal for a particular set of two or more of the plurality of transmitRF chains includes information from only the one respective particulartransmit symbol stream.

At least one or more of the RF connections may be selectable RFconnections that selectively couple certain of the plurality ofdirective gain antenna elements to certain of the plurality of transmitRF chains, and wherein the number of directive gain antenna elementsthat can be selectively coupled to transmit RF chains may exceed thenumber of transmit RF chains that can provide transmit RF signals to theone or more selectable RF connections.

At least one of the directive gain antenna elements that can beselectively coupled to transmit RF chains may also be one of thedirective gain antenna elements that can be selectively coupled toreceive RF chains.

All of the directive gain antenna elements that can be selectivelycoupled to transmit RF chains may also be directive gain antennaelements that can be selectively coupled to receive RF chains.

None of the plurality of directive gain antenna elements that can becoupled to the plurality of transmit RF chains may also be a directivegain antenna element that can be coupled to any receive RF chain.

The number of directive gain antenna elements that can be coupled to theplurality of transmit RF chains may equal the number of transmit RFchains.

The antenna array may further include a plurality of transmit poweramplifiers, wherein each transmit power amplifier can be coupled to atleast one of the plurality of transmit RF chains and to at least one ofthe plurality of directive gain antenna elements that can be coupled tothe plurality of transmit RF chains.

At least two or more of the directive gain antenna elements that can becoupled to transmit RF chains may be oriented in different directions toprovide directional diversity.

The set of directive gain antenna elements that can be coupled totransmit RF chains may include directive gain antenna elements of atleast two different orthogonal polarizations.

The set of the directive gain antenna elements that can be coupled totransmit RF chains may be divided between one subset with a firsttransmit polarization and a second subset with a second transmitpolarization.

The first transmit polarization may be vertical and the second transmitpolarization may be horizontal.

The first transmit polarization may be left-hand circular and the secondtransmit polarization may be right-hand circular. The set of transmit RFchains that can provide transmit RF signals to the one or more RFconnections may be divided between one subset that provides transmit RFsignals to directive gain antenna elements with the first transmitpolarization and a second subset that provides transmit RF signals todirective gain antenna elements with the second transmit polarization.

At least two of the directive gain antenna elements that can be coupledto transmit RF chains may be each arranged on separate respective facetsamongst a plurality of facets with one or more directive gain antennaelements per facet, and each facet may be oriented at a different anglein the azimuth relative to at least one other facet.

At least one of the directive gain antenna elements that can be coupledto transmit RF chains may be arranged on a facet with no directive gainantenna element that can be coupled to any receive RF chain.

All of the directive gain antenna elements that can be coupled totransmit RF chains may be arranged on one or more facets each with nodirective gain antenna element that can be coupled to any receive RFchain.

The radio resource controller may set or cause to be set the specificselective couplings between the certain of the plurality of directivegain antenna elements and the certain of the plurality of transmit RFchains.

The radio resource controller may set or cause to be set the specificselective couplings between the certain of the plurality of directivegain antenna elements and the certain of the plurality of transmit RFchains such that the directive gain antenna elements selectively coupledto transmit RF chains for a transmit superframe are those selectivelycoupled to receive RF chains in an immediately preceding receivesuperframe.

Each of the one or more modulator cores may include at least oneencoder; at least one symbol grouper; and at least one symbol mapper.

At least one of the one or more modulator cores may produce at least twotransmit symbol streams and such at least one of the one or moremodulator cores may further include a stream parser, interposed betweenthe transmit data interface and the at least two symbol groupers, tosplit a stream of data within the modulator core into two or moresub-streams.

Each of the one or more modulator cores may further include at least onescrambler.

Each of the one or more modulator cores may further include at least oneinterleaver.

Each of the one or more demodulator cores may include at least onedecoder; and at least one soft decision symbol demapper.

At least one of the one or more demodulator cores may demodulatee atleast two receive symbol streams and wherein such at least one of theone or more demodulator cores may further include a stream multiplexer,interposed between the receive data interface and the at least two softdecision symbol demappers, to combine two or more sub-streams of datawithin the demodulator core into a single stream.

Each of the one or more demodulator cores may further include at leastone descrambler.

Each of the one or more demodulator cores may further include at leastone deinterleaver.

The transmit path channel multiplexer may operate on one or moresuccessive blocks of symbols from the one or more transmit symbolstreams and the transmit path channel multiplexer may include at leastone cyclic prefix adder that prepends a fraction of the block oftransmit chain time domain samples to be transmitted sequentially lastin time to such block to produce a cyclically-extended block of transmitchain time domain samples.

The transmit path channel multiplexer may further include at least onetransmit channel equalizer. Each transmit channel equalizer may producetransmit chain channel-equalized symbols by applying respectivestream-specific and chain-specific transmit weights to the successiveblocks of symbols from the one or more transmit symbol streams coupledto each transmit channel equalizer.

The respective stream-specific and chain-specific transmit weightsapplied to the successive blocks of symbols from the one or moretransmit symbol streams may vary with relative symbol position withinsuch blocks.

The relative symbol position may represent a particular frequencycomponent of the transmit chain input signal.

The frequency selective receive path channel multiplexer may operate onone or more successive blocks of samples from the plurality of receivechain output signals and the frequency selective receive path channelmultiplexer may include a plurality of respective cyclic prefix removersthat discard a fraction of the samples within the one or more successiveblocks of samples from the plurality of respective receive chain outputsignals corresponding to a known cyclic prefix length for a set of oneor more transmit symbol streams expected to be present within theplurality of receive chain output signals; a complex Discrete FourierTransformer coupled to each respective cyclic prefix remover, whereineach complex Discrete Fourier Transformer decomposes the cyclic prefixremoved one or more successive blocks of samples from the plurality ofreceive chain output signals into a set of receive chain frequencydomain subchannel samples; and one or more receive channel equalizerscoupled to the plurality of complex Discrete Fourier Transformers,wherein each respective receive channel equalizer produces a set ofchannel-equalized frequency domain estimates representative of arespective one of the one or more transmit symbol streams expected to bepresent within the plurality of receive chain output signals by applyingrespective stream-specific and chain-specific receive weights to therespective sets of receive chain frequency domain subchannel samples,and wherein said stream-specific and chain-specific receive weightsapplied to the respective sets of receive chain frequency domainsubchannel samples vary with relative frequency domain subchannelposition within such sets.

The intelligent backhaul radio may further include a channel equalizercoefficients generator, wherein the channel equalizer coefficientsgenerator determines the stream-specific and chain-specific receiveweights that vary with relative frequency domain subchannel positionbased on comparison of sets of receive chain frequency domain subchannelsamples with the expected samples corresponding to known blocks oftraining pilots associated with each of the one or more transmit symbolstreams expected to be present within the plurality of receive chainoutput signals.

The stream-specific and chain-specific transmit weights may also bedetermined by the channel equalizer coefficients generator.

A respective block of training pilots from a pilot symbol library withinor coupled to the transmit path channel multiplexer may be selectivelyapplied to each of the one or more transmit symbol streams.

A pilot symbol library within or coupled to the transmit path channelmultiplexer may supply pilot symbols for selective insertion atpredetermined positions within certain successive blocks of symbols fromthe one or more transmit symbol streams.

A respective block of training pilots from a pilot data library withinor coupled to one or more modulator cores may be selectively applied toeach of the one or more transmit symbol streams.

A pilot data library within or coupled to one or more modulator coresmay supply pilot data for selective insertion at predetermined positionswithin certain successive blocks of symbols from the one or moretransmit symbol streams.

Preamble symbols from a preamble symbol library within or coupled to thetransmit path channel multiplexer may be selectively applied to at leastone of the one or more transmit symbol streams.

Preamble samples from a preamble samples library within or coupled tothe transmit path channel multiplexer may be selectively applied to atleast one of the plurality of transmit chain input signals.

The intelligent backhaul radio may further include anacquisition/synchronization detector. The acquisition/synchronizationdetector may provide symbol boundary and block boundary timingreferences.

The intelligent backhaul radio may further include an interface bridgeconfigured to couple the intelligent backhaul radio to a data network,the interface bridge including one or more Ethernet interfaces to couplethe interface bridge to the data network, the interface bridgemultiplexing and buffering the one or more Ethernet interfaces; and amedia access controller to exchange data to and from the data networkvia coupling to at least the interface bridge and to and from at leastone other intelligent backhaul radio via coupling to at least the one ormore modulator cores and the one or more demodulator cores, wherein themedia access controller outputs transmit data to a transmit path andinputs receive data from a receive path.

The data network may be a remote data network. The data network may be acore data network.

The intelligent backhaul radio may further include a transmit physicallayer convergence protocol generator; and a receive physical layerconvergence protocol analyzer. The transmit physical layer convergenceprotocol generator, interposed between the media access controller andthe one or more modulator cores, may prepend or append additionalinformation bits to the transmit data outputted by the media accesscontroller in the process of composing the one or more transmit datainterface streams to the one or more modulator cores. The receivephysical layer convergence protocol analyzer, interposed between themedia access controller and the one or more demodulator cores, maydetect and analyze additional information bits prepended or appendedwithin the one or more receive data interface streams provided by theone or more demodulator cores in the process of composing the receivedata inputted to the media access controller.

The intelligent backhaul radio may further include a radio linkcontroller, wherein the radio link controller sets or causes to be setcertain modulation mapping or forward error correction encodingparameters for the one or more modulator cores.

The radio link controller may set or cause to be set certain parameterswithin the plurality of transmit RF chains or a plurality of transmitpower amplifiers each coupled to a respective transmit RF chain relatedto the transmitted signal power from the intelligent backhaul radio.

The radio link controller may compose or cause to be composed a controlframe to be sent via the media access controller to another radio linkcontroller in another intelligent backhaul radio.

The radio resource controller may compose or cause to be composed acontrol frame to be sent via the media access controller to anotherradio resource controller in another intelligent backhaul radio.

The intelligent backhaul radio may further include an intelligentbackhaul management system agent that sets or causes to be set certainpolicies relevant to the radio resource controller, wherein theintelligent backhaul management system agent exchanges information withother intelligent backhaul management system agents within otherintelligent backhaul radios or with one or more intelligent backhaulmanagement system servers.

According to another aspect of the invention, an intelligent backhaulradio is disclosed that includes one or more demodulator cores, whereineach demodulator core demodulates one or more receive symbol streams toproduce a respective receive data interface stream, each of the one ormore demodulator cores including at least one decoder; and at least onesoft decision symbol demapper. The intelligent backhaul radio alsoincludes a plurality of receive RF chains to convert from a plurality ofreceive RF signals to a plurality of respective receive chain outputsignals. The intelligent backhaul radio also includes a frequencyselective receive path channel multiplexer, interposed between the oneor more demodulator cores and the plurality of receive RF chains, toproduce the one or more receive symbol streams provided to the one ormore demodulator cores from the plurality of receive chain outputsignals wherein the frequency selective receive path channel multiplexeroperates on one or more successive blocks of samples from the pluralityof receive chain output signals and the frequency selective receive pathchannel multiplexer includes a plurality of respective cyclic prefixremovers that discard a fraction of the samples within the one or moresuccessive blocks of samples from the plurality of respective receivechain output signals corresponding to a known cyclic prefix length for aset of one or more transmit symbol streams expected to be present withinthe plurality of receive chain output signals; a plurality of complexDiscrete Fourier Transformers, each complex Discrete Fourier Transformercoupled to each respective cyclic prefix remover, wherein each complexDiscrete Fourier Transformer decomposes the cyclic prefix removed one ormore successive blocks of samples from the plurality of receive chainoutput signals into a set of receive chain frequency domain subchannelsamples; and one or more receive channel equalizers coupled to theplurality of complex Discrete Fourier Transformers, wherein eachrespective receive channel equalizer produces a set of channel-equalizedfrequency domain estimates representative of a respective one of the oneor more transmit symbol streams expected to be present within theplurality of receive chain output signals by applying respectivestream-specific and chain-specific receive weights to the respectivesets of receive chain frequency domain subchannel samples, and whereinsaid stream-specific and chain-specific receive weights applied to therespective sets of receive chain frequency domain subchannel samplesvary with relative frequency domain subchannel position within suchsets. The intelligent backhaul radio also includes one or more modulatorcores, wherein each modulator core modulates a respective transmit datainterface stream to produce one or more transmit symbol streams whereineach of the one or more modulator cores includes at least one encoder;at least one symbol grouper; and at least one symbol mapper. Theintelligent backhaul radio also includes a plurality of transmit RFchains to convert from a plurality of transmit chain input signals to aplurality of respective transmit RF signals. The intelligent backhaulradio also includes a transmit path channel multiplexer, interposedbetween the one or more modulator cores and the plurality of transmit RFchains, to produce the plurality of transmit chain input signalsprovided to the plurality of transmit RF chains from the one or moretransmit symbol streams wherein the transmit path channel multiplexeroperates on one or more successive blocks of symbols from the one ormore transmit symbol streams and the transmit path channel multiplexerincludes at least one cyclic prefix adder that prepends a fraction ofthe block of transmit chain time domain samples to be transmittedsequentially last in time to such block to produce a cyclically-extendedblock of transmit chain time domain samples. The intelligent backhaulradio also includes an antenna array including a plurality of directivegain antenna elements; one or more selectable RF connections thatselectively couple certain of the plurality of directive gain antennaelements to certain of the plurality of receive RF chains, wherein thenumber of directive gain antenna elements that can be selectivelycoupled to receive RF chains exceeds the number of receive RF chainsthat can accept receive RF signals from the one or more selectable RFconnections; and a plurality of RF connections to couple at leastcertain of the plurality of directive gain antenna elements to theplurality of transmit RF chains; wherein at least two or more of thedirective gain antenna elements that can be selectively coupled toreceive RF chains are oriented in different directions to providedirectional diversity, wherein the set of directive gain antennaelements that can be selectively coupled to receive RF chains includedirective gain antenna elements of at least two different orthogonalpolarizations, wherein the set of the directive gain antenna elementsthat can be selectively coupled to receive RF chains is divided betweenone subset with a first polarization and a second subset with a secondpolarization, and wherein the first polarization is vertical and thesecond polarization is horizontal. The intelligent backhaul radio alsoincludes a radio resource controller, wherein the radio resourcecontroller sets or causes to be set the specific selective couplingsbetween the certain of the plurality of directive gain antenna elementsand the certain of the plurality of receive RF chains. The intelligentbackhaul radio also includes an interface bridge configured to couplethe intelligent backhaul radio to a data network, the interface bridgeincluding one or more Ethernet interfaces to couple the interface bridgeto the data network, the interface bridge multiplexing and buffering theone or more Ethernet interfaces. The intelligent backhaul radio alsoincludes a media access controller to exchange data to and from the datanetwork via coupling to at least the interface bridge and to and from atleast one other intelligent backhaul radio via coupling to at least theone or more modulator cores and the one or more demodulator cores,wherein the media access controller outputs transmit data to a transmitpath and inputs receive data from a receive path. The intelligentbackhaul radio also includes a radio link controller, wherein the radiolink controller sets or causes to be set certain modulation mapping orforward error correction encoding parameters for the one or moremodulator cores.

The first polarization may be left-hand circular and the secondpolarization may be right-hand circular.

The set of receive RF chains that can accept receive RF signals from theone or more selectable RF connections may be divided between one subsetthat accepts receive RF signals from directive gain antenna elementswith the first polarization and a second subset that accepts receive RFsignals from directive gain antenna elements with a second polarization.

The directive gain antenna elements that can be selectively coupled toreceive RF chains may be arranged on a plurality of facets with one ormore directive gain antenna elements per facet, and each facet may beoriented at a different angle in the azimuth relative to at least oneother facet. The one or more selectable RF connections may be arrangedsuch that any receive RF chains that can accept receive RF signals fromthe one or more selectable RF connections can be selectively coupled todirective gain antenna elements from more than one facet. The one ormore selectable RF connections may be arranged such that the set ofreceive RF chains that can accept receive RF signals from the one ormore selectable RF connections can be selectively coupled to directivegain antenna elements from any two facets sharing a common projectededge. The one or more selectable RF connections may be arranged such theset of receive RF chains that can accept receive RF signals from the oneor more selectable RF connections can be selectively coupled todirective gain antenna elements from any two facets closest to eachother in azimuthal angle amongst all facets including directive gainantenna elements that can be selectively coupled to receive RF chains.Each facet may include directive gain antenna elements of at least twodifferent orthogonal polarizations.

The number of transmit RF chains may equal the number of transmit symbolstreams.

The transmit path channel multiplexer may couple the plurality oftransmit RF chains to respective transmit symbol streams such that eachrespective transmit chain input signal includes information from onlyone respective transmit symbol stream.

The number of transmit RF chains may exceed the number of transmitsymbol streams, and wherein transmit path channel multiplexer may coupleat least one set of two or more of the plurality of transmit RF chainsto a particular transmit symbol stream such that each transmit chaininput signal for a particular set of two or more of the plurality oftransmit RF chains includes information from only the one respectiveparticular transmit symbol stream.

The set of the plurality of directive gain antenna elements that can becoupled to the plurality of transmit RF chains may be different than theset of the plurality of directive gain antenna elements that can becoupled to the plurality of receive RF chains.

The number of directive gain antenna elements that can be coupled to theplurality of transmit RF chains may equal the number of transmit RFchains.

The antenna array may further include a plurality of transmit poweramplifiers, wherein each transmit power amplifier can be coupled to atleast one of the plurality of transmit RF chains and to at least one ofthe plurality of directive gain antenna elements that can be coupled tothe plurality of transmit RF chains.

At least two or more of the directive gain antenna elements that can becoupled to transmit RF chains may be oriented in different directions toprovide directional diversity.

The set of directive gain antenna elements that can be coupled totransmit RF chains may include directive gain antenna elements of atleast two different orthogonal polarizations.

The set of the directive gain antenna elements that can be coupled totransmit RF chains may be divided between one subset with a firsttransmit polarization and a second subset with a second transmitpolarization. The first transmit polarization may be vertical and thesecond transmit polarization may be horizontal. The set of transmit RFchains that can provide transmit RF signals to the one or more RFconnections may be divided between one subset that provides transmit RFsignals to directive gain antenna elements with the first transmitpolarization and a second subset that provides transmit RF signals todirective gain antenna elements with the second transmit polarization.

At least two of the directive gain antenna elements that can be coupledto transmit RF chains may be each arranged on separate respective facetsamongst a plurality of facets with one or more directive gain antennaelements per facet, and each facet may be oriented at a different anglein the azimuth relative to at least one other facet.

At least one of the directive gain antenna elements that can be coupledto transmit RF chains may be arranged on a facet with no directive gainantenna element that can be coupled to any receive RF chain.

The directive gain antenna elements that can be coupled to transmit RFchains may be arranged on one or more facets, and the one or more facetsdo not include a directive gain antenna element that can be coupled to areceive RF chain.

At least one of the one or more modulator cores may produce at least twotransmit symbol streams and such at least one of the one or moremodulator cores may further include a stream parser, interposed betweenthe transmit data interface and the at least two symbol groupers, tosplit a stream of data within the modulator core into two or moresub-streams.

At least one of the one or more demodulator cores may demodulate atleast two receive symbol streams and such at least one of the one ormore demodulator cores may further include a stream multiplexer,interposed between the receive data interface and the at least two softdecision symbol demappers, to combine two or more sub-streams of datawithin the demodulator core into a single stream.

The intelligent backhaul radio may further include a channel equalizercoefficients generator, wherein the channel equalizer coefficientsgenerator determines stream-specific and chain-specific receive weightsthat vary with relative frequency domain subchannel position based oncomparison of sets of receive chain frequency domain subchannel sampleswith the expected samples corresponding to known blocks of trainingpilots associated with each of the one or more transmit symbol streamsexpected to be present within the plurality of receive chain outputsignals.

A respective block of training pilots from a pilot symbol library withinor coupled to the transmit path channel multiplexer may be selectivelyapplied to each of the one or more transmit symbol streams.

A pilot symbol library within or coupled to the transmit path channelmultiplexer may supply pilot symbols for selective insertion atpredetermined positions within certain successive blocks of symbols fromthe one or more transmit symbol streams.

A respective block of training pilots from a pilot data library withinor coupled to one or more modulator cores may be selectively applied toeach of the one or more transmit symbol streams.

A pilot data library within or coupled to one or more modulator coresmay supply pilot data for selective insertion at predetermined positionswithin certain successive blocks of symbols from the one or moretransmit symbol streams.

The data network may be a remote data network.

The data network may be a core data network.

The radio link controller may set or cause to be set certain parameterswithin the plurality of transmit RF chains or a plurality of transmitpower amplifiers each coupled to a respective transmit RF chain relatedto the transmitted signal power from the intelligent backhaul radio.

The radio link controller may compose or cause to be composed a controlframe to be sent via the media access controller to another radio linkcontroller in another intelligent backhaul radio.

The radio resource controller may compose or cause to be composed acontrol frame to be sent via the media access controller to anotherradio resource controller in another intelligent backhaul radio.

The intelligent backhaul radio may further include an intelligentbackhaul management system agent that sets or causes to be set certainpolicies relevant to the radio resource controller, wherein theintelligent backhaul management system agent exchanges information withother intelligent backhaul management system agents within otherintelligent backhaul radios or with one or more intelligent backhaulmanagement system servers.

In additional embodiments, an intelligent backhaul radio (IBR) may becombined in operation with, a part of or the entirety of, an ancillaryradio to form a hybrid intelligent backhaul radio (HB-IBR). Theancillary radio and the IBR radio operate in different bands. Forexample, the HB-IBR may include an IBR operating in a non-line of sightmode of operation within the 5.8 GHz unlicensed band, and the ancillaryradio link may operate in the F.C.C. §101 E Band. In one embodiment, theancillary radio is, part of or the entirety of, a conventional point topoint back haul radio (CBR). In another embodiment, the ancillary radiois, part of or the entirety of, another intelligent back haul radio(IBR). In some embodiments, the HB-IBR is a combination of a NLOS(non-line of sight) radio and a nLOS (near line of sight) or LOS (lineof sight) radio.

The E Band provides distinct advantages for use in deploying point topoint wireless data links in that the channels of operation allow forsignificantly higher occupied bandwidths by the modulation signal,resulting in higher rate data links. Additionally, there is generallyless opportunity for interference to and from other co-channel stationswithin the E Band resulting in a simplified FCC licensing process.

However, the E Band also provides distinct disadvantages for use in theoperation of a point to point radio link. Two of these disadvantagesinclude the cost of installation due to the requirement of highlyskilled technicians, and the robustness of operation of the point topoint link due to variations in structure or operational conditions ofthe link and/or equipment. An additional disadvantage is that suchinstalled links are not self-healing (i.e., are not reactive to suchvariations of conditions and equipment parameters).

In one particular embodiment, the HB-IBR includes a 5.8 GHz Part 15 linkand a E Band Part 101 link. This configuration of the HB-IBR providesthe specific advantages of the E Band radio link, but also overcomes thedisadvantages associated with the existing E band point to point backhaul radios.

In some embodiments, the aforementioned advantages may be achieved byspecific coordination in signaling over the two point to point links.For example, the NLOS (non-line-of sight, 5.8 GHz) link may be used forthe transport of control frames, acknowledgment frames (or negativeacknowledgement frames), and/or the like, while the nLOS (near line ofsight) or LOS (line of sight) link in the E Band may be used primarilyor entirely for transport of the data payload. Such control frames mayprovide all of the antenna control messaging or metrics feedback for thepurpose of antenna control at the transmitting-Band link radio, whichcan be used to adjust and/or optimize the antenna operation (i.e., theradio is self-healing). Other control signaling may include use ofsignaling between MAC, RLC, or RRC entities for any purpose discussed asa function within the IBR embodiments within this disclosure. In someembodiments, the modulation and coding scheme (MCS) may be signaled,while in others coordination of operational frequencies may beperformed, while in yet other embodiments, coordination ofretransmissions of data received in error may be signaled. Oneparticularly useful embodiment of such coordinated signaling is for usewhen adaptive transmitter beam forming is utilized within an IBR pointto point E-band link, coordinated and managed utilizing the NLOS link.An alternative but related embodiment includes using the NLOS link toaid in the alignment of the nLOS link by providing metrics or commandsfor use in the control of a servo or otherwise motorized alignmentmechanizing as known in the art. Such servo motors may be used toperform adjustments to the azimuth or elevation of a fixed dish typeantenna for the nLOS or LOS link, allowing for the NLOS link to aid inperforming an initial or continually optimization of the nLOS or LOSlink.

In some embodiments, the radios in the HB-IBR may share a common MAC anddistinctly separate RRC, RLC, MODEM, and associated radio blocks. Inother embodiments, the radios in the HB-IBR may be entirely separate,but with a coordinating function between the MAC entities for each radioat each respective HB-IBR site.

The HB-IBR provides significant advantages relative to current E BandCBRs, including a reduced installation time for the equipment and pointto point link configuration. In addition, the cost of installation isdecreased because the required proficiency of the individuals performingthe installation is lower. In particular, the number of individualsrequired to perform the installation may be reduced. In addition, therequired skill level of the individuals performing the installation maybe reduced. In addition, the precision of the alignment of the nLOSfixed antennas may be greatly simplified and may even be performedremotely in some cases.

In some embodiments, a more optimal initial installation may beperformed, in which a ‘survey” of various reception parameters may beused as an optimization metric, at each of the motorized nLOS or LOSradios to determine the most robust, highest performance or mostotherwise optimum alignment of the nLOS or LOS links antennas. In someembodiments, performance of the HB-IBR may be improved because initialoperating parameters (e.g., antenna positions) may be selected so thatthe link performances are less susceptible to variations in theinstallation or operating environment (e.g., structure vibration,temperature changes, rain fades, etc.).

In some embodiments, the control and coordination between the NLOS andnLOS/LOS links allow for a self-healing capability (allowing for thenLOS/LOS link to be continually optimized). Such optimization may beuseful in conditions where a nLOS link is modified by the growth oftrees, or their structural changes to the propagation environment.

Additional benefits of embodiments of the HB-IBR include a reducedlatency of the payload on the LOS link when the LOS link is operated inTDD mode, and when the NLOS link is utilized for the signaling for theneed for re-transmissions (ACK/NACK), allowing for a faster response todropped radio FEC blocks. This is the result of not requiring the delayin sending the ACK/NAK signaling of the time division duplexed (TDD)return path on the LOS link.

In some embodiments, the HB-IBR allows for a redundant data linkcapability for high priority traffic. For example, in the case of a LOSor nLOS link outage, specific classifications of QOS packets or otherpackets may be sent over the lower data rate NLOS link, while otherclassifications of packets may be either queued or discarded. Suchembodiments ensure the most critical traffic continues to be delivered,while less critical traffic may be delayed or undelivered. Such trafficclassification may be based on, for example, MPLS, 802.1p, DSRC,IntServ, DifServ, or other related QOS, priority, or otherclassification schemes as known in the art.

BRIEF DESCRIPTION OF THE DRAWINGS

The accompanying drawings, which are incorporated into and constitute apart of this specification, illustrate one or more examples ofembodiments and, together with the description of example embodiments,serve to explain the principles and implementations of the embodiments.

FIG. 1 is an illustration of conventional point to point (PTP) radiosdeployed for cellular base station backhaul with unobstructed line ofsight (LOS).

FIG. 2 is a block diagram of a conventional PTP radio for Time DivisionDuplex (TDD).

FIG. 3 is a block diagram of a conventional PTP radio for FrequencyDivision Duplex (FDD).

FIG. 4 is an illustration of a MAC Protocol Data Unit (MPDU).

FIG. 5 is an illustration of intelligent backhaul radios (IBRs) deployedfor cellular base station backhaul with obstructed LOS according to oneembodiment of the invention.

FIG. 6 is a block diagram of an IBR according to one embodiment of theinvention.

FIG. 7 is a block diagram of an IBR according to one embodiment of theinvention.

FIG. 8 is a block diagram illustrating an exemplary deployment of IBRsaccording to one embodiment of the invention.

FIG. 9 is a block diagram illustrating an exemplary deployment of IBRsaccording to one embodiment of the invention.

FIG. 10 is a block diagram of an IBR antenna array according to oneembodiment of the invention.

FIG. 11 is a block diagram of a front-end unit for TDD operationaccording to one embodiment of the invention.

FIG. 12 is a block diagram of a front-end unit for FDD operationaccording to one embodiment of the invention.

FIG. 13 is a perspective view of an IBR according to one embodiment ofthe invention.

FIG. 14 is a perspective view of an IBR according to one embodiment ofthe invention.

FIG. 15 is a perspective view of an IBR according to one embodiment ofthe invention.

FIG. 16 is a block diagram illustrating an exemplary transmit chainwithin an IBR RF according to one embodiment of the invention.

FIG. 17 is a block diagram illustrating an exemplary receive chainwithin an IBR RF according to one embodiment of the invention.

FIG. 18 is a block diagram illustrating an IBR modem according to oneembodiment of the invention.

FIG. 19 is a block diagram illustrating a modulator core j according toone embodiment of the invention.

FIG. 20 is a block diagram illustrating a demodulator core j accordingto one embodiment of the invention.

FIG. 21 is a block diagram illustrating a modulator core j according toone embodiment of the invention.

FIG. 22 is a block diagram illustrating a demodulator core j accordingto one embodiment of the invention.

FIG. 23 is a block diagram illustrating a channel multiplexer (MUX)according to one embodiment of the invention. FIG. 23A shows thetransmit path and the channel equalizer coefficients generator withinthe exemplary channel MUX. FIG. 23B shows the receive path within theexemplary channel MUX.

FIG. 24 is a block diagram illustrating an exemplary Tx-CE-m accordingto one embodiment of the invention.

FIG. 25 is a block diagram illustrating an exemplary Rx-CE-1 accordingto one embodiment of the invention.

FIG. 26 is a timing diagram illustrating processing of PPDU-l withTx-path and Rx-path of respective IBR channel MUXs according to oneembodiment of the invention.

FIG. 27 is a block diagram illustrating an exemplary Tx PLCP accordingto one embodiment of the invention.

FIG. 28 is a block diagram illustrating an exemplary Tx PLCP Mod-jaccording to one embodiment of the invention.

FIG. 29 is a block diagram illustrating an exemplary Rx PLCP accordingto one embodiment of the invention.

FIG. 30 is a block diagram illustrating an exemplary Rx PLCP Mod-jaccording to one embodiment of the invention.

FIG. 31 is a schematic diagram of an IBR communications protocols stackaccording to one embodiment of the invention.

FIG. 32 is a schematic diagram of an IBR communications protocols stackaccording to one embodiment of the invention.

FIG. 33 is a block diagram of an IBR media access control (MAC)according to one embodiment of the invention.

FIG. 34 is a timing diagram illustrating channel activity for FDD withfixed superframe timing according to one embodiment of the invention.

FIG. 35 is a timing diagram illustrating channel activity for TDD withfixed superframe timing according to one embodiment of the invention.

FIG. 36 is a timing diagram illustrating channel activity for TDD/CSMAwith variable superframe timing according to one embodiment of theinvention.

FIG. 37 is a block diagram illustrating a Hybrid Band Intelligent Backhaul radio (HB-IBR) according to one embodiment of the invention.

FIG. 38 is a flow diagram illustrating an HB-IBR installation processaccording to one embodiment of the invention

FIG. 39 is a timing and message flow diagram illustrating the timing ofsignals for an embodiment of a HB-IBR with a TDD E Band (n)LOS link anda 5.8 GHz ISM link according to one embodiment of the invention.

FIG. 40 is a block diagram illustrating a Hybrid Band Intelligent BackHaul radio (HB-IBR) utilizing a CBR and a IBR according to oneembodiment of the invention.

FIG. 41 is a block diagram of a hybrid band intelligent backhaul radioutilizing an electronically steerable antenna array for the upper bandaccording to one embodiment of the invention.

FIG. 42 is illustrates a physical configuration of an HB-IBR antennaconfiguration utilizing a dish antenna for the upper band according toone embodiment of the invention.

FIG. 43 illustrates a physical configuration of an HB-IBR antennaconfiguration utilizing an electronically steerable antenna array forthe upper band according to one embodiment of the invention.

FIG. 44 illustrates a physical arrangement of the upper band antennaarray having composite sub-array and sub-array panels according to oneembodiment of the invention.

FIG. 45 is a block diagram of the transmission phased array componentsand control signals for the electronically steerable antenna arrayaccording to one embodiment of the invention.

DETAILED DESCRIPTION

FIG. 5 illustrates deployment of intelligent backhaul radios (IBRs) inaccordance with an embodiment of the invention. As shown in FIG. 5, theIBRs 500 are deployable at street level with obstructions such as trees504, hills 508, buildings 512, etc. between them. The IBRs 500 are alsodeployable in configurations that include point to multipoint (PMP), asshown in FIG. 5, as well as point to point (PTP). In other words, eachIBR 500 may communicate with more than one other IBR 500.

For 3G and especially for 4^(th) Generation (4G), cellular networkinfrastructure is more commonly deployed using “microcells” or“picocells.” In this cellular network infrastructure, compact basestations (eNodeBs) 516 are situated outdoors at street level. When sucheNodeBs 516 are unable to connect locally to optical fiber or a copperwireline of sufficient data bandwidth, then a wireless connection to afiber “point of presence” (POP) requires obstructed LOS capabilities, asdescribed herein.

For example, as shown in FIG. 5, the IBRs 500 include an Aggregation EndIBR (AE-IBR) and Remote End IBRs (RE-IBRs). The eNodeB 516 of the AE-IBRis typically connected locally to the core network via a fiber POP 520.The RE-IBRs and their associated eNodeBs 516 are typically not connectedto the core network via a wireline connection; instead, the RE-IBRs arewirelessly connected to the core network via the AE-IBR. As shown inFIG. 5, the wireless connection between the IBRs include obstructions(i.e., there may be an obstructed LOS connection between the RE-IBRs andthe AE-IBR).

FIGS. 6 and 7 illustrate exemplary embodiments of the IBRs 500 shown inFIG. 5. In FIGS. 6 and 7, the IBRs 500 include interfaces 604, interfacebridge 608, MAC 612, modem 624, channel MUX 628, RF 632, which includesTx1 . . . TxM 636 and Rx1 . . . RxN 640, antenna array 648 (includesmultiple antennas 652), a Radio Link Controller (RLC) 656 and a RadioResource Controller (RRC) 660. The IBR may optionally include an IBMSagent 700 as shown in FIG. 7. It will be appreciated that the componentsand elements of the IBRs may vary from that illustrated in FIGS. 6 and7. The various elements of the IBR are described below by theirstructural and operational features in numerous different embodiments.

The external interfaces of the IBR (i.e., the IBR Interface Bridge 608on the wireline side and the IBR Antenna Array 648 (including antennas652) on the wireless side) are a starting point for describing somefundamental differences between the numerous different embodiments ofthe IBR 500 and the conventional PTP radios described above (or othercommonly known radio systems, such as those built to existing standardsincluding 802.11n (WiFi) and 802.16e (WiMax)).

In some embodiments, the IBR Interface Bridge 608 physically interfacesto standards-based wired data networking interfaces 604 as Ethernet 1through Ethernet P. “P” represents a number of separate Ethernetinterfaces over twisted-pair, coax or optical fiber. The IBR InterfaceBridge 608 can multiplex and buffer the P Ethernet interfaces 604 withthe IBR MAC 612. For the case of P=1 (a single Ethernet interface), themultiplexing operation of the IBR Interface Bridge 608 is a trivial“pass-through” between the single Ethernet interface and the buffer. Inexemplary embodiments, the IBR Interface Bridge 608 preserves “Qualityof Service” (QoS) or “Class of Service” (CoS) prioritization asindicated, for example, in IEEE 802.1q 3-bit Priority Code Point (PCP)fields within the Ethernet frame headers, such that either the IBR MAC612 schedules such frames for transmission according to policiesconfigured within the IBR of FIG. 6 or communicated via the IBMS Agent700 of FIG. 7, or the IBR interface bridge 608 schedules the transfer ofsuch frames to the IBR MAC 612 such that the same net effect occurs. Inother embodiments, the IBR interface bridge 608 also forwards andprioritizes the delivery of frames to or from another IBR over aninstant radio link based on Multiprotocol Label Switching (MPLS) orMultiprotocol Label Switching Transport Profile (MPLS-TP).

In some embodiments, the IBR Interface Bridge 608 can also perform layer2 switching of certain Ethernet interfaces to other Ethernet interfaces604 in response to radio link failure conditions and policies configuredwithin the IBR of FIG. 6 or communicated via the IBMS Agent 700 of FIG.7. A radio link failure condition can arise from any one or more ofmultiple possible events, such as the following exemplary radio linkfailure condition events:

physical failure of a component within the IBR other than the IBRInterface Bridge and its power supply;

degradation of the RF link beyond some pre-determined throughput leveldue to either changing propagation environment or additional co-channelinterference; and

failure of any kind at the other end of the RF link that preventsconnection to the ultimate source or destination.

FIG. 8 illustrates an exemplary configuration of multiple IBRs (IBR 1 1804, IBR 2 808). Each IBR 804, 808 has layer 2 switching in the IBRinterface bridges 816, 820 (each corresponding to an instance of the IBRInterface Bridge 608 of FIGS. 6 and 7). In one embodiment, the datanetworking traffic can be from, for example, a cellular eNodeB, a WiFihotspot, a enterprise edge router, or any of numerous other remote datanetworks 828. As shown in FIG. 8, the remote data network 828 isconnected via an Ethernet cable (copper or fiber) 832 to the firstEthernet port 836 on the IBR Interface Bridge 816 of IBR1 804. AnotherEthernet cable 840 connects the second Ethernet port 844 on the IBRInterface Bridge 816 of IBR1 804 to the first Ethernet port 848 on theIBR Interface Bridge 820 of IBR2 808. If a radio link failure conditionoccurs for any reason, such as those listed above, with respect to RFLink 1 852, then the layer 2 switch within the IBR Interface Bridge 816of IBR1 804 can automatically connect all data networking trafficoriginating from or destined to Remote Data Network 1 828 via IBR2 808and RF Link2 856, completely transparently to Remote Data Network 1 828.This provides fail over redundancy to reduce the probability of networkoutage at Remote Data Network 1 828.

In some embodiments, the IBR Interface Bridge with layer 2 switching canalso be configured to perform load balancing in response to operatingconditions and policies configured within the IBR of FIG. 6 orcommunicated via the IBMS Agent 700 of FIG. 7. For example, withreference to FIG. 8, the layer 2 switch in the IBR Interface Bridge 816of IBR1 804 can connect all data networking traffic in excess of datarates above a certain limit, such as a pre-determined level or theinstantaneous supportable rate on RF Link 1 852, over to IBR2 808. Forfull two-way functionality of this load balancing, an analogous loadbalancing capability exists within the layer 2 switch of an IBR at therespective other ends of both RF Link 1 852 and RF Link 2 856.

FIG. 9 illustrates an alternative configuration of IBRs 804, 808 withlayer 2 switching capability and optional load balancing capability forthe case of two disparate Remote Data Networks 1 and 2 (900 and 904,respectively). The two Remote Data Networks 1 and 2 (900 and 904) are ator within Ethernet cabling distance of two IBRs 1 and 2 (804, 808)operating on two RF links 1 and 2 (852, 856). As described above, theRemote Data Network 828 is connected via Ethernet cable 832 to the firstEthernet port 836, and the IBRs 1 and 2 (804, 808) are connected viaEthernet cable 840 at Ethernet ports 844 and 848 respectively. TheRemote Data Network 2 904 is connected to IBR 2 808 via Ethernet cable908 at the Ethernet port 912. In the embodiment shown in FIG. 9, if aradio link failure condition occurs for any reason, such as those listedabove, with respect to RF Link 1 852, then the IBR Interface Bridge 816of IBR1 804 can use its layer 2 switch to connect to the IBR InterfaceBridge 820 of IBR2 808 via Ethernet cable 840 such that IBR2 808 canbackhaul, subject to its throughput capabilities and prioritizationpolicies, the traffic originating from or destined to both Remote DataNetwork 1 900 and Remote Data Network 2 904. Similarly, the IBRs 804,808 can perform load balancing across both RF Links 1 and 2 (852, 856),for traffic originating from or destined to Remote Data Networks 1 and 2(900, 904).

In some embodiments, RF link 1 852 may utilize spectrum possessingadvantageous conditions, such as reduced interference, wider channelbandwidth, better propagation characteristics, and/or higher allowablepower than the spectrum utilized by RF Link 2 856, or vice versa. In thesituation where a radio link failure condition occurs with respect tothe more advantageous spectrum, either control signaling between the twoIBR Interface Bridges 816, 820 of IBRs 1 and 2 as shown in FIG. 6 ormessaging between the two IBMS Agents 700 as shown in FIG. 7, whetherdirectly or indirectly via one or more intermediaries, can cause theredundant IBR 808 to change to the advantageous spectrum no longer beingused by RF Link 852 with the failure condition.

FIG. 10 illustrates an exemplary embodiment of an IBR Antenna Array 648.FIG. 10 illustrates an antenna array having Q directive gain antennas652 (i.e., where the number of antennas is greater than 1). In FIG. 10,the IBR Antenna Array 648 includes an IBR RF Switch Fabric 1012, RFinterconnections 1004, a set of Front-ends 1008 and the directive gainantennas 652. The RF interconnections 1004 can be, for example, circuitboard traces and/or coaxial cables. The RF interconnections 1004 connectthe IBR RF Switch Fabric 1012 and the set of Front-ends 1008. EachFront-end 1008 is associated with an individual directive gain antenna652, numbered consecutively from 1 to Q.

FIG. 11 illustrates an exemplary embodiment of the Front-end circuit1008 of the IBR Antenna Array 648 of FIG. 10 for the case of TDDoperation, and FIG. 12 illustrates an exemplary embodiment of theFront-end circuit 1008 of the IBR Antenna Array 648 of FIG. 10 for thecase of FDD operation. The Front-end circuit 1008 of FIG. 11 includes atransmit power amplifier PA 1104, a receive low noise amplifier LNA1108, SPDT switch 1112 and band-select filter 1116. The Front-endcircuit 1008 of FIG. 12 includes a transmit power amplifier PA 1204,receive low noise amplifier LNA 1208, and duplexer filter 1212. Thesecomponents of the Front-end circuit are substantially conventionalcomponents available in different form factors and performancecapabilities from multiple commercial vendors.

As shown in FIGS. 11 and 12, each Front-end 1008 also includes an“Enable” input 1120, 1220 that causes substantially all active circuitryto power-down. Power-down techniques are well known. Power-down isadvantageous for IBRs in which not all of the antennas are utilized atall times. It will be appreciated that alternative embodiments of theIBR Antenna Array may not utilize the “Enable” input 1120, 1220 orpower-down feature. Furthermore, for embodiments with antenna arrayswhere some antenna elements are used only for transmit or only forreceive, then certain Front-ends (not shown) may include only thetransmit or only the receive paths of FIGS. 11 and 12 as appropriate.

As described above, each Front-end (FE-q) corresponds to a particulardirective gain antenna 652. Each antenna 652 has a directivity gain Gq.For IBRs intended for fixed location street-level deployment withobstructed LOS between IBRs, whether in PTP or PMP configurations, eachdirective gain antenna 652 may use only moderate directivity compared toantennas in conventional PTP systems at a comparable RF transmissionfrequency. Based on measurements of path loss taken at street level at2480 MHz in various locations in and nearby San Jose, Calif. duringAugust and September 2010, IBR antennas should have a Gq of at least 6dBi, and, in typical embodiments for operation between 2 GHz and 6 GHzRF transmission frequency, a Gq in the range of 10-18 dBi, wherein theradiation pattern in the elevation direction is typically less than 90°and nominally parallel to the local surface grade. At higher RFtransmission frequencies, higher gain ranges of Gq are expected to bepreferable. For example, Gq may be preferably 16-24 dBi for 20-40 GHzoperation or 20-28 dBi for 60-90 GHz operation. In one particularembodiment, the directive gain antennas 652 are “patch” type antennaswith Gq of about 13 dBi and nominally equal elevation and azimuthradiation patterns (about 40° each). Patch type antennas areadvantageous because they can be realized using substantiallyconventional printed circuit board (PCB) fabrication techniques, whichlowers cost and facilitates integration with Front-end circuitcomponents and/or some or substantially all of the IBR RF Switch Fabric.However, may other antenna types, such as helical, horn, and slot, aswell as microstrip antennas other than patch (such as reflecteddipoles), and the like, may be used with the IBR Antenna Array. In analternative embodiment, the directive gain antennas 652 are reflecteddipoles with Gq of about 15 dBi (about 50° azimuth and 20° elevation).In many embodiments, the antenna elements are chosen with elevationangular patterns considerably less than azimuthal angular patterns.

In the IBR Antenna Array 648 illustrated in FIGS. 6, 7 and 10, the totalnumber of individual antenna elements 652, Q, is greater than or equalto the larger of the number of RF transmit chains 636, M, and the numberof RF receive chains 640, N. In some embodiments, some or all of theantennas 652 may be split into pairs of polarization diverse antennaelements realized by either two separate feeds to a nominally singleradiating element or by a pair of separate orthogonally orientedradiating elements. Such cross polarization antenna pairs enable eitherincreased channel efficiency or enhanced signal diversity as describedfor the conventional PTP radio. The cross-polarization antenna pairs aswell as any non-polarized antennas are also spatially diverse withrespect to each other.

In some embodiments, certain antenna elements 652 may be configured withdifferent antenna gain Gq and/or radiation patterns compared to othersin the same IBR to provide pattern diversity.

In some embodiments, some antenna elements 652 may be oriented indifferent ways relative to others to achieve directional diversity. Forexample, FIG. 13 illustrates an IBR suitable for obstructed LOS PTPoperation (or sector-limited PMP operation) in which spatial diversity(and optionally polarization diversity and/or pattern diversity) isutilized to the exclusion of directional diversity. As shown in FIG. 13,all of the antenna elements 1304 are positioned on a front facet 1308 ofthe IBR. In FIG. 13, the IBR 1300 includes eight antenna elements 1304(Q=8). It will be appreciated that the IBR 1300 may include less than ormore than eight antenna elements 1304.

FIG. 14 illustrates another embodiment of an IBR 1400 where directionaldiversity is present. IBR 1400 includes the same number of antennaelements as the IBR 1300 shown in FIG. 13 (Q=8, or 16 if usingcross-polarization feeds to all antenna elements). In FIG. 14, theantenna elements 1404 are arranged on a front facet 1408 and two sidefacets 1412. In FIG. 14, the side facets 1412 are at a 45° angle in theazimuth relative to the front facet 1408. It will be appreciated thatthis 45° angle is arbitrary and different angles are possible dependingon the specific radiation patterns of the various antenna elements.Furthermore, the angle may be adjustable so that the side facets 1412can vary in azimuth angle relative to the front facet between 0° to 90°(any value or range of values between 0° to 90°). Conventionalelectromechanical fabrication elements could also be used to make thisside facing angle dynamically adjustable by, for example, the RRC 660 ofFIG. 6 or the same in combination with the IBMS Agent 700 of FIG. 7.Additionally, variations of the embodiment of FIG. 14 can use more thanthree facets at different angular spacing all within a nominal azimuthalrange of approximately 180°, and the number of antenna elements 1404 maybe less than or greater than Q=8. For example, in one embodiment, theantenna array includes four facets uniformly distributed in an azimuthalangular range across 160°.

FIG. 15 illustrates an IBR 1500 having an “omni-directional” (in theazimuth) array of antenna elements 1504. In FIG. 15, Q=16 antennaelements 1504 are uniformly distributed across all 360° of azimuthangles, amongst the eight facets 1508-1536. Such an embodiment can beadvantageous for propagation environments with severe obstructionsbetween IBRs in a radio link or for an omni-directional common node at apoint of aggregation (i.e. fiber POP) within a PMP deployment of IBRs.It will be appreciated that the IBR may have less than or more thaneight facets, and that the number of antenna elements 1504 may be lessthan or greater than Q=16. It will also be appreciated that the antennaelements 1504 may be distributed non-uniformly across the facets.

With reference back to FIGS. 10-12, the IBR RF Switch Fabric 1012provides selectable RF connections between certain RF-Tx-m and/orRF-SW-Tx-q combinations and certain RF-Rx-n and/or RF-SW-Rx-qcombinations. In an embodiment where Q=M=N, the IBR RF Switch Fabric1012 can be parallel through connections or single-pole, single-throw(SPST) switches. In a maximally flexible embodiment where Q>Max (M, N)and any RF-Tx-m or RF-Rx-n can connect to any respective RF-SW-Tx-q orRF-SW-Rx-q, then a relatively complex cascade of individual switchblocks and a more extensive decoder logic may be required. Because eachRF-Tx-m or RF-Rx-n can be readily interchangeable amongst theirrespective sets of signals at the digital baseband level, it isgenerally only necessary to connect any given RF-Tx-m or RF-Rx-n to asubset of the Front-ends 1008 roughly by the ratio respectively of Q/Mor Q/N on average.

For example, if the IBR has Q=8 antenna elements and M=N=4, thenQ/M=Q/N=2. Thus, any of the RF-Tx-m (m=1, 2, 3, 4) signals may beconnectable to a pair of RF-SW-Tx-q signals, via a selectable RFconnection including a SPDT switch (and similarly for RF-Rx-n toRF-SW-Rx-q). In this example, either RF-Tx-m and/or RF-Rx-n couldconnect via such a selectable RF connection to either one of thefront-facing antenna elements or one of the side-facing antenna elementssuch that each RF signal has directional as well as spatial diversityoptions while allowing any two adjacent elements in the azimuthdirection to both be selected. Similarly, for the IBR shown in FIG. 15,if the IBR has Q=16 (non-polarized) antenna elements and M=N=4, then anyRF-Tx-n or RF-Rx-n signal could be oriented in one of four directions at90° increments via a selectable RF connection including a single-pole,quadrature throw (SP4T) switch.

An alternative embodiment of the IBR RF Switch Fabric 1012 can alsooptionally connect, via a signal splitter, a particular RF signal(typically one of the RF-Tx-m signals) to multiple Front-ends 1008 andantenna elements 652 simultaneously. This may be advantageous in someIBR operational modes to provide an effectively broader transmitradiation pattern either in normal operation or specifically for certainchannel estimation or broadcast signaling purposes. In context of theSPDT switch implementation in the example above for the IBR of FIG. 14,this would entail, if used for RF-Tx-m, the addition of another SPDTswitch and three passive splitter/combiners as well as decoder logic foreach antenna element pair.

In all of the foregoing descriptions of the IBR RF Switch Fabric 1012,substantially conventional components and RF board design structures asare well known can be used to physically implement such selectable RFconnections. Alternatively, these selectable RF connections can also berealized by custom integrated circuits on commercially-availablesemiconductor technologies.

With reference back to FIGS. 6 and 7, the IBR RF 632 also includestransmit and receive chains 636, 640. Exemplary transmit and receivechains 636, 640 are shown in FIGS. 16 and 17 respectively. In oneembodiment, as shown in FIG. 16, the transmit chain 636 takes a transmitchain input signal such as digital baseband quadrature signals I_(Tm)and Q_(Tm) and then converts them to a transmit RF signal RF-Tx-m.Typically, each transmit chain Tx-m 636 includes at least two signalDACs, channel filters, a vector modulator, a programmable gainamplifier, an optional upconverter, and at least one synthesized LO.Similarly, as shown in FIG. 17, the receive chain 640 converts a receiveRF signal RF-Rx-n to a receive chain output signal such as digitalbaseband quadrature signals I_(Rn) and Q_(Rn). Typically, each receivechain Rx-n 640 includes an optional downconverter, a vector demodulator,an AGC amplifier, channel filters, at least two signal ADCs and at leastone synthesized LO. A common synthesized LO can often be shared betweenpairs of Tx-m and Rx-n chains, or even amongst a plurality of suchpairs, for TDD operation IBRs. Examples of commercially availablecomponents to implement the IBR RF chains include the AD935x family fromAnalog Devices, Inc. Numerous other substantially conventionalcomponents and RF board design structures are well known as alternativesfor realizing the Tx-m and/or Rx-n chains whether for TDD or FDDoperation of the IBR.

With reference back to FIGS. 6 and 7, the specific details of the IBRModem 624 and IBR Channel MUX 628 depend somewhat on the specificmodulation format(s) deployed by the IBR. In general, the IBR requires amodulation format suitable for a broadband channel subject tofrequency-selective fading and multipath self-interference due to thedesired PHY data rates and ranges in obstructed LOS propagationenvironments. Many known modulation formats for such broadband channelsare possible for the IBR. Two such modulation formats for the IBR are(1) Orthogonal Frequency Division Multiplexing (OFDM) and (2)Single-Carrier Frequency Domain Equalization (SC-FDE). Both modulationformats are well known, share common implementation elements, and havevarious advantages and disadvantages relative to each other.

As is well known, OFDM essentially converts the frequency-selectivefading broadband channel into a parallel collection of flat-fadingsubchannels wherein the frequency spacing between subchannels is chosento maintain orthogonality of their corresponding time domain waveforms.In OFDM, a block of information symbols is transmitted in parallel on ablock of discrete frequency subchannels, each conveying one informationsymbol which can be efficiently channel multiplexed into the time domainby using an Inverse Discrete Fourier Transform (IDFT). A cyclic prefixof length in time greater than the dominant time delays associated withmulti-path self-interference is then pre-pended to the IDFT output blockby serially transmitting first in time a fraction of the IDFT outputblock time domain samples that are transmitted last. This length in timeis also sometimes called a guard interval. The use of a cyclic prefixeffectively converts a linear convolution of the transmitted block ofsymbols to a circular convolution such that the effects of inter-symbolinterference (ISI) associated with multipath time delays can be largelyeliminated at the OFDM receiver. At the OFDM receiver, the cyclic prefixis discarded and each time domain input block of symbols isdemultiplexed back into frequency domain subchannels each conveying oneinformation symbol by using a Discrete Fourier Transform (DFT). Thetransmission of a known training block of symbols within each OFDM PPDUenables the OFDM receiver to correct for carrier frequency offsets anddetermine a complex weighting coefficient for each frequency subchannelthat can equalize the effects of frequency-selective relative gain andphase distortion within the propagation channel. Furthermore,transmission of known “pilot” sequences of symbols at certainpredetermined subchannels within the transmit block enables the OFDMreceiver to track such channel distortions and frequency offsets duringreception of information symbol blocks the PPDU as well as provide acoherent reference for demodulation. Note that for those subchannelssubjected to severe flat fading, as will occur inevitably in a broadbandobstructed LOS propagation channel, the information within suchsubchannels cannot be directly demodulated. Thus to avoid a significantirreducible bit-error rate (BER) that would be unacceptable for most IBRapplications, it is essential that either forward error correction (FEC)encoding be applied with a constraint length comparable to the number ofbits per OFDM block of information symbols or with a combination ofconstraint length and interleaving depth such that related FEC encodedbits or symbols span substantially all of the OFDM block of informationsymbols.

In an SC-FDE transmitter, every block of information symbols, eachmapped to the same single carrier frequency at a relatively high symbolrate, has a cyclic prefix prepended to it prior to transmission. Similarto OFDM, the cyclic prefix consists of a finite fraction of themodulated symbols with a length in time greater than the dominant timedelays associated with multipath self-interference wherein suchmodulated symbols are identical to those to be transmitted last in timefor each block. Analogously to OFDM, this cyclic prefix effectivelyconverts a linear convolution of the transmitted block of symbols to acircular convolution such that inter-block interference (IBI) due tomultipath can be largely eliminated at the SC-FDE receiver. The SC-FDEreceiver is similar to the OFDM receiver in that a cyclic prefix removerdiscards a cyclic prefix for each block of information symbols and theremaining sampled signals are decomposed into a set of frequencysubchannels collectively representing the IBI-free block of symbolsusing a DFT. Based on a set of complex weighting coefficients, one foreach frequency sub-channel, as usually determined from a known trainingblock of symbols within each SC-FDE PPDU, the broadband channel inducedrelative distortions of amplitude and phase for each frequencysub-channel are then corrected in the Frequency Domain Equalizer (FDE).In contrast to OFDM where FDE-corrected subchannel estimates can bedirectly demapped as individual information symbols, in SC-FDE theFDE-corrected frequency domain subchannel estimates are thenre-multiplexed into a channel equalized single-carrier stream ofinformation symbol estimates using an IDFT so that such informationsymbol estimates can be subsequently demodulated.

Embodiments of the IBR may use Quadrature Amplitude Modulation (QAM) tomap groups of information data bits to a symbol including an I (or“real”) component and a Q (or “imaginary”) component. These symbols(i.e., symbols that include I and Q components) are typically referredto as “complex” symbols. Such “complex” symbols may be multiplexed ordemultiplexed by an IDFT or DFT respectively implemented by structuresexecuting a complex Inverse Fast Fourier Transform (IFFT) or complexFast Fourier Transform (FFT). In IBR embodiments, references to IDFT orDFT herein assume that such transforms will typically be implemented bystructures executing an IFFT or FFT respectively. Note also that thecyclic prefix described above can also be implemented as a cyclicpostfix for either OFDM or SC-FDE with equivalent performance. ForSC-FDE, some re-ordering of samples at the receiver after removal duringthe guard interval may be required if a cyclic postfix is used. It willbe appreciated however that techniques other than QAM for modulationmapping may also be used.

With reference again to FIGS. 6 and 7, the specific details of the IBRModem 624 and IBR Channel MUX 628 also depend somewhat on the specificantenna array signal processing format(s) deployed by the IBR. Ingeneral, the IBR utilizes multiple antennas and transmit and/or receivechains which can be utilized advantageously by several well-knownbaseband signal processing techniques that exploit multipath broadbandchannel propagation. Such techniques include Multiple-Input,Multiple-Output (MIMO), MIMO Spatial Multiplexing (MIMO-SM), beamforming(BF), maximal ratio combining (MRC), and Space Division Multiple Access(SDMA).

In general, any configuration where a transmitter that has multipletransmit antennas (or “inputs” to the propagation channel) communicateswith a receiver that has multiple receive antennas (or “outputs” fromthe propagation channel) can technically be described as MIMO. However,typically the term MIMO is used in the context of spatially multiplexingmultiple encoded and modulated information streams from multipletransmit antennas into a multipath channel for receipt at multiplereceive antennas wherein inversion of channel transfer matrix, usuallydetermined by a known training block associated with each PPDU, enablesseparation and demodulation/decoding of each information stream—aprocess called MIMO-SM. Various embodiments of the IBR, as describedherein, advantageously use other types of antenna diversity such asdirectional or polarization diversity to realize MIMO-SM performanceeven in propagation environments where spatial separation alone may beinadequate for conventional MIMO-SM.

For a given encoded and modulated information stream, BF or MRC can beutilized at either the transmitter or the receiver (or both) to improveeither the signal to interference and noise ratio (SINR) or the signalto noise ratio (SNR). For example, BF or MRC optimally combine theinformation signal received from the multiple antennas or split theinformation stream signal as transmitted by the multiple antennas.Numerous algorithms for determining the optimal weighting criteriaamongst the multiple antennas, usually as a function of frequency withina frequency-selective multipath broadband channel, are well known.

SDMA allows an Aggregation End IBR (AE-IBR) in a PMP configuration (seeFIG. 5) to transmit to or receive from multiple Remote End IBRs(RE-IBRs) simultaneously using parallel encoded and modulatedinformation streams each associated with multiple antenna andtransmit/receive chain combinations wherein stream-specific BF maximizessignal quality for a given stream and IBR pair, while minimizinginterference to other streams and IBR pairs. To the extent that multipleRE-IBRs are separable in space, or another antenna array characteristicsuch as polarization or direction, then significant increases in overallspectrum efficiency of a PMP system are possible using SDMA. As with BF(and MRC), numerous algorithms for computing the optimal weightingcriteria, such as Eigen Beam Forming (EBF), amongst multiple antennasare well known.

In view of the foregoing exemplary modulation format and antenna arrayprocessing format alternatives for the IBR, exemplary embodiments of theIBR Modem 624 and IBR Channel MUX 628 are described with reference toFIGS. 18-30.

FIG. 18 shows an exemplary embodiment of the IBR Modem 624. The IBRmodem 624 includes a Tx PLCP generator 1804, an Rx PLCP analyzer 1808,multiple modulator cores 1812 and multiple demodulator cores 1816. FIG.18 is divided functionally into a transmit path and a receive path. Thetransmit path includes the TxPLCP 1804 and the modulator cores 1812, andthe receive path includes the Rx PLCP analyzer 1808 and the demodulatorcores 1816.

The transmit path of the IBR Modem 624 includes a total of Jmod“Modulator Cores” 1812, each denoted as Modulator Core j wherein j=1, 2,. . . , Jmod. The Tx PLCP generator 1804 provides transmit datainterface streams, Tx-j, to each Modulator Core j 1812 such that Ajtotal vector outputs of mapped transmit symbol streams (denoted by the“+” on such I, Q connections) are generated from each Modulator Core j1812. This results in a total number of transmit symbol streams,K=A1+A2+ . . . +AJmod, each in vector format (I_(m), Q_(TS))_(k) fromk=1 to K that are connected to the transmit path of the IBR Channel MUX628.

Similarly, the receive path of the IBR Modem 624 includes a total ofJdem “Demodulator Cores” 1816 each denoted as Demodulator Core j 1816wherein j=1, 2, . . . , Jdem. The IBR Channel MUX receive path providesL=B1+B2+ . . . +BJdem vector format receive symbol streams (I_(RS),Q_(RS))_(l) for l=1 to L that are input as Bj vector streams per eachDemodulator Core j 1816 to produce the receive data interface streamRx-j.

In PTP IBR configurations where Jmod=Jdem, usually Aj=Bj. However, for aPTP IBR where probing capability is present, Aj=Bj only for j=1 to Jmodin cases where Jdem>Jmod. In PMP IBR configurations, it may happen thatAj≠Bj; even if Jmod=Jdem.

An exemplary embodiment of a Modulator Core j 1812 is illustrated inFIG. 19. As shown in FIG. 19, this exemplary modulator core 1812includes a scrambler 1908, encoder 1912, stream parser 1916, multipleoptional interleavers 1920, multiple symbol groupers 1924 and multiplesymbol mappers 1928.

Typically, the data from the Tx PLCP generator 1804, Tx-j 1904, isscrambled at the scrambler 1908 and then passed to the encoder 1912. Theencoder 1912 provides FEC encoding and in some types of encoders alsoeffectively interleaves the encoded data. Exemplary FEC encoder typesfor IBRs include convolutional, turbo and low density parity check(LDPC). The encoded data is passed to the Stream Parser 1916. The StreamParser 1916 demultiplexes the encoded data into Aj streams. Each encodeddata stream is then interleaved if necessary at the optionalinterleavers 1920 such that the greater of the FEC encoder constraintlength and the interleaving depth approximates the total number of bitsper transmitted block of symbols in either OFDM or SC-FDE. Exampleinterleaver types include block (or “row/column”) and convolutional.Such interleaved and/or encoded data in each stream is then grouped atsymbol groupers 1924 based on the number of encoded bits per symbol. Thegroups of bits pass to the symbol mapper 1928, which converts each groupof encoded bits into a vector representation (I, Q) within aconstellation and then provides an output as a transmit symbol stream1932. An exemplary technique for mapping encoded bits to a vector symbolis QAM optionally with Gray coding.

FIG. 20 illustrates an exemplary embodiment of a Demodulator Core j 1816compatible with the exemplary Modulatory Core j 1812 of FIG. 19. Asshown in FIG. 20, the demodulator core 1816 includes a descrambler 2008,decoder 2012, stream MUX 2016, multiple optional deinterleavers 2020,and multiple soft decision symbol demappers 2024.

The Demodulator Core j 1816 at the highest level can be described asperforming essentially the reverse operations of those performed in theModulator Core j 1812 of FIG. 19. A key difference though is that thevector representation (I, Q) receive symbol streams 2032 input to eachDemodulator Core j 1816 are only estimates which may be corrupted due tochannel or receiver impairments such as multipath self-interference,Gaussian noise, co-channel interference, carrier frequency offset (CFO),distortion through channel filters at Tx and/or Rx, non-linearity in theTx and/or Rx chains and Front-ends, or phase noise in either Tx and/orRx local oscillators. Thus, the Demodulator Core j 1816 may use the softdecision symbol demapper 2024, which estimates the likelihood that areceived symbol or bit has a particular value using, for example, aknown technique such as Log-Likelihood Ratio (LLR). For example, if eachdata bit out of the demapper 2024 had a soft-decision representation (or“metric”) of 8 bits, then a value of 0 would represent a data bit of 0,a value of 1-20 would indicate most likely a data bit of 0, a value of21-125 would indicate more likely a data bit of 0 than a data bit of 1,a value of 126-129 would indicate near uncertainty of the data bit aseither 0 or 1, a value of 130-234 would indicate more likely a data bitof 1, a value of 235-254 would indicate most likely a data bit of 1, anda value of 255 would represent a data bit of 1. These soft-decisionmetrics can then be deinterleaved if applicable at optionaldeinterleavers 2020 and stream multiplexed at the Stream MUX 2016, andthen supplied to the decoder (deinterleaver) 2012 as a sequence ofsoft-decision metrics estimating the originally encoded (and possiblyinterleaved) bit stream. Decoder types are matched to encoder types asis well known. Techniques such as iterative decoding within the IBRmodem or combination of IBR modem and IBR Channel MUX are also known andcan be used in some embodiments.

FIGS. 19 and 20 are examples of implementations of the modulator anddemodulator cores 1812, 1816, respectively, in the IBR Modem 624. Itwill be appreciated that the order of the Scrambler 1908 and Encoder1912 can be reversed (and hence the Decoder 2012 and Descrambler 2008could be reversed). Also, the Stream Parser 1916 can divide a transmitdata interface stream Tx-j sequentially into multiple encoder/scramblercombinations and hence the corresponding Stream Mux 2016 would combinemultiple Decoder outputs. FIGS. 21 and 22 illustrate exemplaryalternatives with the above recited differences and without showingoptional separate interleavers 1920 and deinterleavers 2020.

Although each element is illustrated separately in FIGS. 19-22, theelements are not required to be distinct physical structures. It isfeasible to time multiplex either the entire Modulator or DemodulatorCores 1816, 1820 or constituent elements such as the Encoder 1912 orDecoder 2012 across multiple streams. Furthermore, in TDD operation, itcan be advantageous to time multiplex constituent elements such as theEncoder 1912 and/or Decoder 2012 even during times where the oppositetransmit/receive path is over the air compared to the time multiplexedelement. For example, by buffering receive symbol stream samples fromthe receive path of the IBR Channel MUX 628 during the receive portionof TDD operation, some of the streams can be decoded in a common Decoder2012 even when the IBR has changed over to transmit operation.

Note further that the exemplary embodiments of FIGS. 19-22 for theModulator and Demodulator Cores of the IBR Modem are all suitable foreither OFDM or SC-FDE operation.

FIG. 23 (FIGS. 23A and 23B together) illustrates an exemplary embodimentof the IBR Channel MUX 628. FIG. 23 is divided functionally into atransmit path (FIG. 23A) and a receive path (FIG. 23B). In FIG. 23A, thetransmit path includes multiple block assemblers 2304, multiple transmitchannel equalizers (CEs) 2308, multiple transmit MUXs 2312, multiplecyclic prefix addition (CPA) and block serializers 2316, multipletransmit digital front ends (DFEs) 2320, an optional preamble sampleslibrary 2324, and a pilot (and optionally preamble) symbol library 2328.In FIG. 23B, the receive path includes an acquisition/synchronizationcalculator 2336, multiple receive digital front ends (DFEs) 2340,multiple cyclic prefix removal (CPR) and block assemblers 2344, multiplecomplex DFTs 2348, multiple receive channel equalizers 2352 and multiplereceive MUXs 2356. The IBR Channel MUX 628 also includes a channelequalizer coefficients generator 2332 (see FIG. 23A). The channelequalizer coefficients generator 2332 may be used by both transmit andreceive paths or only the receive path depending on the specificembodiment. In the receive path, the IBR Channel MUX 628 is frequencyselective to enable operation in obstructed LOS propagation environmentswith frequency selective fading within the channel bandwidth as well asoperation in predominantly unobstructed LOS.

In the transmit path, each transmit symbol stream of mapped symbols(I_(TS), Q_(TS))_(k) from k=1 to K 2360 is connected to a respective TxBlock Assembler k 2304 as shown in FIG. 23A. For OFDM modulation, eachTx block Assembler k 2304 is equivalent to a serial to parallel bufferthat also places “running” pilot symbols in pre-determined locationscorresponding to pilot subchannels. In the exemplary embodiment of FIG.23A, such pilot symbols are supplied to each Tx Block Assembler k 2304by a Pilot Symbol Library 2328. Alternatively, pilot symbols areselectively injected into the data stream at predetermined points with aModulator Core 1812 similar to FIG. 19 or 21 but with a “Pilot DataLibrary” (not shown) providing grouped data to a selectable buffer ormultiplexer (not shown) between the Symbol Grouper 1924 and SymbolMapper 1928 of either FIG. 19 or 21.

For SC-FDE modulation with no frequency selective channel equalization,the Tx Block Assembler k 2304 would, as an exemplary embodiment, be asimple serial to parallel buffer that places pilot symbols inpre-determined symbol sequence positions either from the Pilot SymbolLibrary 2328 as shown, or alternatively from a “Pilot Data Library” inthe Modulator Core as described above. If frequency selective channelequalization in Tx for SC-FDE is used, then in addition to the above,the Tx Block Assembler k 2304 would also include a Complex DFT thatfollows the serial to parallel buffer. In this DFT structure version ofSC-FDE (also known as DFT pre-coding SC-DFE), it is also possible toinsert the pilot symbols as “pseudo-subchannels” after the DFT operationinstead of as time domain symbols before the DFT.

After block assembly, the blocks of mapped symbols (each a vector of (I,Q) constellation points) are typically supplied to each of M transmitchannel equalizers 2308 (“Tx-CE-m” for m=1 to M in FIG. 23A). EachTx-CE-m 2308 applies K blocks of amplitude and/or phase weights (eachamplitude phase weight may be represented in Cartesian form as a“complex” weight with a “real” and “imaginary” sub-component values)respectively to each of the K blocks of mapped vector symbols.

An exemplary embodiment of a transmit channel equalizer Tx-CE-m 2308 isshown in FIG. 24. The blocks of mapped vector symbols are {right arrowover (TxBlock)}_(k) wherein each symbol element within the vectorTxBlockk has an (I, Q) or, relative to FIG. 24, “complex” value (Irepresenting a “real” sub-component value, Q representing an “imaginary”sub-component value). Each {right arrow over (TxBlock)}_(k) vector ofcomplex symbols is then complex multiplied by a respective transmitweight vector {right arrow over (WT)}_(m,k) as shown in FIG. 24. Thechannel equalized vector of symbols for each transmit chain m is then{right arrow over (TxBlockEq)}_(m) (the transmit chain channel-equalizedsymbols) which represents the complex summation of the symbol by symboloutput vectors of each respective weighting operation. Note that FIG. 24depicts an exemplary implementation of transmit channel equalizerTX-CE-m 2308 based on vector complex multiplication and summation. Suchan approach is easily implemented using either generic function calls orcustom software modules executing on an embedded processor (or DigitalSignal Processor—“DSP”). However, numerous other implementationtechniques are also known such as dedicated logic circuits for complexmultiplication and/or summation, a set of four scalar multipliercircuits and two scalar adders, or other logic circuits such ascombinatorial gates (i.e. OR, NOR, AND, NAND, XOR, XNOR, etc.),multiplexers, shift registers, etc. that can produce an equivalentresult.

Note further that for embodiments with either OFDM or SC-FDE modulationand no frequency selective channel equalization, {right arrow over(WT)}_(m,k) would typically be composed of a block of identical transmitweights applied equally to all mapped symbols for a given stream k. Insome OFDM or SC-FDE embodiments where K=M, no equalization or weightingamongst transmit streams and chains may be desired such that eachTx-CE-m 2308 in FIG. 23A (or FIG. 24) is equivalent to a throughconnection mapping each {right arrow over (TxBlock)}_(k) directly toeach {right arrow over (TxBlockEq)}_(m) for each k=m.

For each transmit chain Tx-m, the channel equalized vector of symbolsfor each transmit chain {right arrow over (TxBlockEq)}_(m) is suppliedto Tx-Mux-m 2312, where m=1 to M, as shown in FIG. 23A. In the case ofOFDM modulation or SC-FDE modulation with frequency-selective channelequalization, each TX-Mux-m 2312 includes an IDFT to transform thesuccessive frequency domain symbols into a block of time domain samples.For SC-FDE modulation with no frequency selective channel equalization,and hence no DFT pre-coding within each Tx Block Assembler k 2304, then{right arrow over (TxBlockEq)}_(m) is already effectively a block oftransmit chain time domain samples and no such IDFT is required.

With reference back to FIG. 23A, each respective Tx-Mux-m 2312 isfollowed by a CPA and Block Serializer-m 2316. “CPA” refers to “CyclicPrefix Addition”-cyclic prefix was described above—which is performed bythe cyclic prefix adder within each CPA and Block Serializer-m 2316.Each CPA and Block Serializer-m 2316, via a cyclic prefix adder,typically replicates a set of samples from the end of the block andprepends these samples to the beginning of a cyclically-extended blockor includes logic to read out these samples in a way that produces anequivalent result. The CPA and Block Serializer-m 2316, via a blockserializer, then effectively performs a parallel to serial conversion ofthe extended block into a sequence of cyclically-extended (I, Q)transmit chain time domain samples.

The cyclically-extended block of (I, Q) time domain samples for eachtransmit chain Tx-m are then supplied to a respective Tx-DFE-m 2320 (DFErefers to Digital Front End). Each Tx-DFE-m 2320 performs a variety ofpossible time domain signal processing operations that may be specificto particular IBR embodiments. Common DFE processes in the transmit pathinclude digital up-conversion of the sampling rate, DC offsetcalibration for each Tx-m transmit chain, digital pre-distortion toaccount for non-linearities in the analog transmit path, pulse-shapingfiltering, crest factor or peak to average power ratio (PAPR) reduction,or frequency shifting to an “intermediate Frequency” (IF) suitable foranalog up conversion to RF-Tx-m in the Tx-m transmit chain (as opposedto the baseband (I_(T), Q_(T))_(m) interface illustrated in FIG. 16).Except for the last listed option of digital IF up conversion, theoutput (a transmit chain input signal) of each respective Tx-DFE-m 2320is typically a sequence of cyclically-extended blocks of calibrated,compensated and filtered baseband symbol samples (I_(T), Q_(T))_(m).

In the receive path of the exemplary IBR Channel MUX 628, downconvertedand amplified samples from I and Q ADCs in each Rx-n receive chain (areceive chain output signal) are passed to respective Rx-DFE-n 2340.Although the receive path of the IBR generally follows the logic ofreversing the operations of the transmit path, the details areconsiderably different in the IBR Channel MUX because in the receivepath the samples are corrupted by channel propagation impairments andarriving at initially unknown times. In view of this the receive pathDigital Front Ends of the IBR Channel MUX shown in FIG. 23B, Rx-DFE-n2340, perform several time domain digital operations typically includingmatched filtering, rotating, sampling rate downconversion, and Rx-nchain calibration. At minimum, the Rx-DFE-n 2340 is used in thedetection of timing synchronization information in the optional Preambleof the L PPDU-l transmissions from the transmitting IBR.

FIG. 26 illustrates this Preamble in the time domain. Note that theoptional Preamble for the l-th Tx-path in a transmitting IBR could beeither generated from a symbol library (as indicated optionally in Pilot(And Preamble) Symbol Library 2328 of FIG. 23) or read directly from aPreamble Samples Library 2324 (also indicated optionally in FIG. 23).

Referring again to FIG. 23B, the Acquisition/Synchronization detector2336 acquires a timing reference, for example, from detection of one ormore of the up to L optional preambles, one or more of the blocks ofTraining Pilots, an optional known pattern within a PLCP header, and/orpilot symbols within blocks of transmit symbol streams. TheAcquisition/Synchronization detector 2336 provides a feedback signal toeach Rx-DFE-n 2340 that enables, for example, symbol rotation andalignment in the time domain (typically in the RX-DFE-n using a CORDICalgorithm). The Acquisition/Synchronization detector 2336 furtherprovides symbol boundary and block boundary timing references (notshown) for use by various elements of the IBR Channel MUX 628 and theIBR Modem 624.

Such corrected receive symbol samples are then supplied to a respectiveCPR and Block Assembler-n 2344. “CPR” means “cyclic prefix removal.” TheCPR and Block Assembler-n 2344 effectively discards the number ofreceived samples at beginning of each block corresponding to the numberof cyclic prefix samples prepended to each block in the transmit path ofthe transmitting IBR. The remaining samples are serial to parallelbuffered into a single block (or an equivalent operation) suitable fordecomposition into receive chain frequency domain subchannels in eachrespective Complex DFT-n 2348.

As shown in FIG. 23B, the sets of receive chain frequency domainsubchannel samples output from the N Complex DFT-n 2348 are collectivelysupplied to L frequency domain receive channel equalizers 2352, each aRx-CE-l. FIG. 25 illustrates an exemplary embodiment of Rx-CE-l 2352.The receive channel equalizer Rx-CE-l 2352 is analogous to the transmitchannel equalizer Tx-CE-m 2308 shown in FIG. 24. Although implementationdetails of each Rx-CE-l 2352 can vary considerably just as describedabove for TX-CE-m 2308, essentially the frequency domain receive vectorsof I and Q samples for each block, {right arrow over (RxBlock)}_(n), arerespectively complex multiplied by complex receive weights {right arrowover (WR)}_(l,n) and then complex summed to produce a set ofchannel-equalized frequency domain estimates, {right arrow over(RxBlockEq)}_(l), representative of the original transmitted blockcorresponding to stream l.

The task of producing such complex receive weight vectors {right arrowover (WR)}_(l,n) that allow each Rx stream l to be separated from themyriad of signals, both desired and undesired, received via N (N≧L)receive chains is performed by the Channel Equalizer CoefficientsGenerator 2332 of FIG. 23A. There are many known algorithms forgenerating the appropriate frequency selective complex receive weightvectors for the IBR Channel MUX as shown in FIG. 23 wherein a known“Training Block” of pilot symbols for each stream l is used to determinethe receive weight vectors {right arrow over (WR)}_(l,n) that allowlinear detection of each {right arrow over (RxBlockEq)}_(l) vector inview of the actual receive chain frequency domain subchannel samplesobserved for the N receive chains during a reception periodcorresponding to transmission of the Training Block (or block ofTraining Pilots). In general, a Channel Equalizer Coefficients Generator2332 that is based on these algorithms calculates the various weights bycomparing the actual receive chain frequency domain subchannel samplesobserved during the reception of the Training Block with the expectedfrequency domain subchannel samples corresponding to a particular knownTraining Block for any given transmit stream. Such algorithms includeZero Forcing (ZF), Maximal Ratio Combining (MRC) and Minimum Mean SquareError (MMSE). Alternatively, other known algorithms for non-lineardetection of each {right arrow over (RxBlockEq)}_(l) are also known,such as Successive Interference Cancellation (SIC) in combination withZF, MRC or MMSE, V-BLAST (an acronym for “vertical Bell Labs LayeredSpace-Time) with ZF or MMSE, or Maximal Likelihood (ML).

The Channel Equalizer Coefficients Generator 2332 also supplies thecomplex transmit weight vectors {right arrow over (WT)}_(m,k) used fortransmit channel equalization within the exemplary IBR Channel MUX 628.In an ideal PTP TDD configuration where K=L, M=N, and no otherco-channel interference beyond the multiple transmit streams, forfrequency domain transmit channel equalization, a straightforwardalternative is to derive {right arrow over (WT)}_(m,k) directly from thecomputed {right arrow over (WR)}_(l,n) of the previous superframe.However, this can be sub-optimal for situations in which a co-channelinterferer, such as for example either another IBR PTP or PMP link inthe same vicinity or a conventional PTP link nearby, affects thereceived signals at the N receive chains of the AE-IBR differently fromthose at the RE-IBR. An alternative is to calculate {right arrow over(WR)}_(l,n) using both MMSE (which will maximize SINR at the receiver)and MRC (which will maximize SNR, or effectively maximize signal power,at the receiver) and then derive {right arrow over (WT)}_(m,k) from thecomputed, but unused in receive channel equalization, {right arrow over(WR)}_(l,n) for MRC. Note that for SC-FDE with no frequency selectivechannel equalization, then the constant {right arrow over (WT)}_(m,k)values applied to all symbols in a {right arrow over (TxBlock)}_(k) canbe blended using known algorithms from vector {right arrow over(WT)}_(m,k) values derived for MRC. This allows such an SC-FDE PTPtransmitter to improve the overall signal quality at the other receiverwhile allowing the other receiver to equalize both interference andfrequency selective fading effects. In view of the foregoing, it isadvantageous for the PMP AE-IBR to use either OFDM or SC-FDE withtransmit frequency selective channel equalization such that the ChannelEqualizer Coefficients Generator can compute MIMO-SDMA complex weights,using for example known EBF or Space Time Adaptive Processing (STAP)algorithms, to minimize multi-stream interference to RE-IBRs thatbeneficially receive only a subset of the transmitted streams. If SC-FDEwithout frequency selective transmit equalization is used, there isstill a benefit in using scalar {right arrow over (WT)}_(m,k) transmitweights at the AE-IBR derived for streams to a given RE-IBR fromprevious superframe MRC at the AE-IBR receiver but some additionalsignal separation such as time and/or frequency may be required todirect data to specific RE-IBRs.

With reference back to FIG. 23B, each respective channel equalized andinterference cancelled symbol samples stream vector {right arrow over(RxBlockEq)}_(l) (or set of channel-equalized frequency domainestimates) is then supplied to an Rx-MUX-l 2356. For OFDM, this istypically a parallel to serial converter that removes the pilotsubchannel symbol samples which are not needed in the IBR Modem. ForSC-FDE, each Rx-MUX-l 2356 includes a Complex IDFT and a parallel toserial converter that removes the time domain symbol samples at thepilot symbol sequence positions. Note though that for IBR embodimentswhere the transmitter uses SC-FDE with frequency selective equalizationand inserts the pilot symbols as “pseudo-subchannels” (see above), eachRx-MUX-l also needs to discard the pilot subchannels prior to theComplex IDFT transformation back to a time domain symbol samples stream.The output of each Rx-MUX-l is a receive symbol stream l that isprovided to a respective input to a demodulator core j.

FIG. 26 illustrates block by block generation of a given transmit symbolstream l in the transmitter IBR as combined into a transmit chain m. Thedesignator “l” is used in FIG. 26 instead of “k” for the transmitter todenote the generation of what becomes the “l-th” receive symbol streambeing demodulated at the receiver. Per the above description of FIG. 23,optionally every PPDU-l can start with a Preamble of known samples thatenables rapid signal acquisition and coarse synchronization. However,for some embodiments of the IBR in either FDD or in TDD with fixed andshort superframe timing, it is not necessary to perform such acquisitionand synchronization from the start of every PPDU. Thus, overhead can beadvantageously minimized by either discarding the Preamble from thePPDU-l generation process, at least for subsequent PPDUs after startup,or effectively combining the desired characteristics of the Preambleinto the Training Block via the Pilots-l. This approach can also be usedwith a Channel Sense Multiple Access (CSMA) approach to MAC schedulingto the extent that a timing master in the system, usually the AE-IBR,maintains sufficiently frequent timing synchronization transmissions.

In some embodiments, the PLCP Header for stream-l is matched to aparticular block such that the modulation and coding scheme (MCS) ofsuch PLCP Header block (see, for example, Block 1 of FIG. 26) is alwayspredetermined and usually chosen to deliver the PLCP header with higherreliability than the data payload blocks to follow. In typicalembodiments, the MCS includes an index number that conveys informationregarding parameters used in the modulation mapping and the forwarderror correction encoding processes. In such embodiments, the PLCPHeader typically conveys at least the information needed to inform thereceiver at the receiving-end IBR of the MCS used for the data payloadblocks to follow. In other embodiments, the MCS or informationindicating an increment, decrement or no change amongst a list ofpossible MCS values is conveyed within Block 0 of FIG. 26 by, forexample, adjusting the modulation of certain pilot symbols (or pilotsubchannels). In the case where Block 1 of FIG. 26 can carry more datathan just the PLCP Header alone, then the IBRs may allocate PPDU payloadto Block 1 even though the bits may be transferred at a different MCSthan that of subsequent Blocks.

In some embodiments, each Block 1 through f (or Block 1 through r) maycorrespond to the output of a block encoder and/or block interleaver ofFIG. 19 or 21. “f” denotes a forward link transmitted from an AE-IBR toan RE-IBR and “r” denotes a reverse link transmitted from an RE-IBR toan AE-IBR. Furthermore, each Block may include error detection bits(such as an FCS) or error correction bits (such as for a Reed-Solomon ora Reed-Muller outer encoder) that can be used either for an AutomaticRepeat reQuest (ARQ) re-transmission protocol of certain blocks or forinput to an RLC and/or RRC entity at either the AE-IBR or RE-IBR tooptimize future link parameters or resource selections.

FIG. 27 illustrates an exemplary embodiment of the Tx PLCP generator1804 of the IBR modem of FIG. 18. As shown in FIG. 27, the Tx PLCPgenerator 1804 includes a Tx PLCP Demux 2704 and multiple Tx PLCPModulators 2708. Based on input from the RRC 660, the Tx PLCP Demux 2704provides data interface streams TxD-j 2716, for j=1 to Jmod, torespective TxPLCP Mod-j 2708 that provide transmit data interfacestreams Tx-j 2720 to a respective Modulator Core j 1812 (shown in FIG.18).

In a PTP IBR configuration, such a plurality of data interface streams2716 and Modulator Cores 1812 may be used, for example, to provide linkdiversity, such as different sets of RLC parameters, carrier frequenciesand/or antenna selections where each set has appropriately multiplexedstreams and chains, or to provide probing capability. In a PMP IBRconfiguration, in addition to the above for PTP, such a plurality ofdata interface streams and Modulator Cores may also be used at an AE-IBRto optimize data transfer to certain RE-IBRs (or groups of RE-IBRs) byusing techniques such as SDMA.

FIG. 28 illustrates an exemplary embodiment of the TxPLCP Mod-j 2708 ofFIG. 27. As shown in FIG. 28, the TxPLCP Mod-j 2708 includes a PLCPheader generator 2804, a PLCP input buffer 2808, a PLCP controller 2812,a training data library 2816, a padding generator 2820 and a PLCPtransmit MUX 2824. In FIG. 28, the PLCP Controller 2812 takes input fromthe RLC and the RRC as well as the current state of the PLCP InputBuffer 2808 to perform “rate matching” for a given PPDU. Rate matchingtypically is used to determine a particular choice of modulation andcoding scheme (MCS) in view of the instantaneous data transfer demandand recent link conditions. In addition to choosing an MCS, the PLCPController 2812 supplies information to the PLCP Header Generator 2804and directs the PLCP Input Buffer 2808 and the Padding Generator 2820 tosupply data to the PLCP Transmit Mux 2824. Depending on the status ofthe RRC and the instantaneous data transfer demand, the PLCP Controller2812 also enables training data from the Training Data Library 2816 tobe multiplexed into a given PPDU as indicated by certain fields in thePLCP Header. Typically, in some embodiments, the PLCP Header conveys atleast the MCS of the PPDU after Block 1, the length of the PPDU payload(for example, either in bytes of payload or in number of blocks pluslength in bytes of padding), the MCS of any training data, the selectedtraining dataset, and the number of training data blocks. Optionally,reply acknowledgements (ACKs) or non-acknowledgements (NACKs) for one ormore previous receive PPDUs corresponding to a companion receive datainterface stream j may also be sent in the PLCP Header. To the extentthat the PLCP also concatenates multiple MPDUs and/or fragments thereof,the PLCP Header Generator also includes sufficient information to allowthe RxPLCP to recover such MPDUs and/or fragments upon receipt. Asdescribed above, FIG. 26 illustrates an exemplary PPDU having a PLCPHeader, a PPDU payload including one or more MPDUs or fragments thereof,and a PAD to cause the PPDU to occupy an integer number of Blocks asshown. Not shown in FIG. 26 is a PPDU extension with one or more Blocksof data from the Training Data Library 2816 of FIG. 28 as may beindicated by the PLCP Header.

Note that for Modulator Cores 1812 that divide each transmit datainterface stream Tx-j into two or more transmit symbol streams, the PLCPHeader of FIG. 28 may be an amalgam of two or more PLCP Headers forrespective transmit symbol streams especially in the case where aseparate MCS applies to each stream (the “vertical encoding” case shownfor example in FIG. 21). Alternatively, a single PCLP Header may be usedper Modulator Core j 1812 with parts of the PLCP Header apportionedamongst two or more transmit symbol streams (the “horizontal encoding”case shown for example in FIG. 19). Another alternative would have asingle PLCP Header encoded and replicated across all transmit symbolstreams of a particular Modulator Core j 1812. In some embodiments, eachPLCP Header further includes an FCS (not shown in FIG. 28) to enable theTx PLCP to determine if the PLCP Header has been demodulated and decodedwithout error. Note also that the PLCP Controller 2812 may be used incertain embodiments to provide or control the provision of timingsignals to the IBR Channel MUX 628 (not shown in FIG. 23) that enableinsertion of either or both of the optional Preamble or of the block ofTraining Pilots as shown in FIG. 26. In exemplary embodiments, a blockof Training Pilots, used, for example, to update transmit and/or receiveweights by the IBR at an opposite end of a link, may be inserted at thebeginning of every transmit superframe, the beginning of every PPDU (asshown in FIG. 26), or at such intervals within a PPDU or superframe asmay be communicated to the Tx PLCP generator 1804 or IBR Channel MUX 628via the RRC 660.

FIG. 29 illustrates an exemplary embodiment of the Rx PLCP analyzer 1808of FIG. 18. As shown in FIG. 29, the Rx PLCP analyzer 1808 includes a RxPLCP MUX 2904 and multiple Rx PLCP Demod-j 2908. In FIG. 29, multiplereceive data interface streams Rx-j each from respective DemodulatorCore j 1812 (see FIG. 18) are input to a respective Rx PLCP Demod-j2908. After removing the respective PLCP Headers, Padding (if any), andTraining Data (if any), each RxD-j is then multiplexed in the RX PLCPMux 2904 and transferred to the IBR MAC 612 as Rx Data 620.

FIG. 30 illustrates an exemplary embodiment of the Rx PLCP Demod-j 2908of FIG. 29. As shown in FIG. 30, the RxPLCP Demod-j 2908 includes a PLCPheader analyzer 3004, a PLCP output buffer 3008, a PLCP controller 3012,a training data analyzer 3016, and a PLCP receive Demux 3024. The PLCPController 3012 may be shared in some embodiments with the PLCPController 2812 of FIG. 28. The Tx or Rx PLCP Controllers 2812, 3012 mayalso be shared across some or all data interface streams. When a PPDU isreceived from a receive data interface stream Rx-j, the PLCP HeaderAnalyzer 3004 filters certain fields from the PLCP Header and sends thisinformation to the PLCP Controller 3012 (or alternatively, is a part ofthe PLCP Controller 3012). This enables the exemplary PLCP Controller3012 to signal the MCS for subsequent symbols or blocks to DemodulatorCore j 1812 as shown in FIG. 30 and to control the PLCP Receive Demux3024 such that the receive data interface stream Rx-j is directed to thePLCP Output Buffer 3008 or Training Data Analyzer 3016 or ignored in thecase of Padding. Further information from the PLCP Header Analyzer 3004and/or PLCP Controller 3012 enables the Training Data Analyzer 3016 todetermine the match between transmitted and received/demodulated/decodedtraining data and communicate certain metrics such as the number of biterrors and the distribution of errors to the RRC 660. In embodimentswhere the PLCP header carries an FCS, the PLCP Header Analyzer 3004 alsochecks the FCS (not shown in FIG. 30) and if a failure occurs, signalsat least the PLCP Controller 3012, the RRC 660, and the RLC 656. ThePLCP Controller 3012 may optionally also inhibit sending RxD-j for theinstant PPDU in the case of such an FCS failure or it may send it onwith an indicator (not shown) to the IBR MAC that such an FCS failurehas occurred.

With reference back to FIGS. 6 and 7, other IBR elements include the IBRMAC 612, the Radio Link Control (RLC) 656, the Radio Resource Control(RRC) 660 and, specific to FIG. 7, the IBMS Agent 700. Although IBRembodiments are possible wherein the MAC 612, RLC 656, RRC 660 and IBMS700 are distinct structural entities, more commonly IBRs are realizedwherein the IBR MAC 612, RLC 656, RRC 660, IBMS 700 and portions of theIBR Interface Bridge 608 are software modules executing on one or moremicroprocessors. Note also that in some IBR embodiments that use of a“Software Defined Radio” (SDR) as the IBR Modem 624 and/or IBR ChannelMUX 628 or portions thereof may also be realized in software executingon one or more microprocessors. Typically in SDR embodiments, the one ormore microprocessors used for elements of the PHY layer are physicallyseparate from those used for the MAC 612 or other layers and arephysically connected or connectable to certain hardware cores such asFFTs, Viterbi decoders, DFEs, etc.

FIGS. 31 and 32 illustrate exemplary views of the IBRs of FIGS. 6 and 7,respectively, showing exemplary communications protocols stacks. It willbe appreciated that some embodiments have the one or more 802.1 MACinstances, the IBR LLC, the IBR MAC, the RRC, the RLC, the IBMS and allother upper layer protocols implemented as software modules or processesexecuting on one or more microprocessors within the IBR.

In accordance with the previous description of the IBR Interface Bridge608, the 802.1 MAC instances of FIGS. 31 and 32 correspond respectivelyto Ethernet interfaces 604 and are substantially conventional. Each802.1 MAC instance is paired with a respective 802.3 PHY instance ofwhich exemplary types include 100 Base-T, 1000 Base-T and variousmembers of the 1000 Base-X family of fiber optic interfaces.

In many exemplary embodiments of the IBR, the IBR Logical Link Control(IBR LLC) layer of FIGS. 31 and 32 is compatible with IEEE 802.2. Inaccordance with the previous description of the IBR Interface Bridge,the IBR LLC layer also uses substantially conventional processes tobridge, for example, 802.2 compatible frames across disparate mediatypes as exemplified by the 802.1, the 802.11 and the IBR MAC layers ofFIGS. 31 and 32. Furthermore, in accordance with the previousdescription of the IBR Interface Bridge, the IBR LLC layer also usessubstantially conventional processes to switch and/or load balance 802.2compatible frames amongst multiple 802.1 MAC instances if available.

FIGS. 31 and 32 depict an exemplary IEEE 802.11 compatible radio (alsoknown as “WiFi”) including 802.11 MAC and 802.11 PHY layers and one ormore antennas. In some IBR embodiments, such an 802.11 radio, which maybe compatible with 802.11b, 802.11a, 802.11g, 802.11n or other 802.11PHY layer variants, within the IBR may be configured as an access point(AP) to allow significant wireless local area network (WLAN) traffic tobe backhauled by the IBR over its wireline or wireless interfaces asappropriate. In some embodiments, the same antennas may be utilized inboth the IBR PHY, which typically includes the IBR Modem 624, IBRChannel MUX 628, IBR RF 632 and IBR Antenna Array 648 in reference toFIGS. 6 and 7, and the 802.11 PHY (e.g., via the IBR RF Switch Fabric ofFIG. 10 (not shown)). Note further that multiple instances of the 802.11radio can also be connected to the IBR LLC in an analogous manner toconnecting multiple Ethernet interfaces.

Another IBR embodiment may provide a more limited 802.11 radiocapability for local configuration purposes (to the exclusion of WLANtraffic and general access). Traditionally PTP and PMP systems haveprovided a “console” input for local configuration via a command lineinterface of radios in the field particularly for situations wherenetwork configuration is either unavailable or undesirable. However,when an IBR is deployed, for example, on a street light, traffic light,building side, or rooftop, a wired console access with a terminal may beextremely inconvenient and/or dangerous. Thus, in some embodiments,802.11 radios are deployed as an access point such that terminalsincluding smartphones, tablets, laptops or other portable computingdevices with 802.11 station capability can connect to such IBRs in sucha console mode. In one embodiment, this deployment is used solely forconfiguration purposes. Configuration by a terminal with 802.11 stationcapability is also possible in the case of one or more 802.11 APsdeployed for WLAN access purposes. Note further that for theconfiguration-only 802.11 AP in an IBR, exemplary embodiments may alsodeploy the 802.11 radio as an Ethernet device on one of the P Ethernetinterfaces depicted in FIGS. 6, 7, 31 and 32, or via some otherIBR-internal wired or bus interface. In such configuration-only 802.11AP IBR embodiments, one or more separate antennas for 802.11 use wouldtypically be provided by the IBR. Furthermore, the configuration-only802.11 interface is not restricted to AP mode only but can also includepeer to peer (“IBSS”), AP mode at the terminal, or WiFi direct.

With reference to FIGS. 31 and 32, typical applications protocols suchas Hyper Text Transfer Protocol (HTTP), Simple Network ManagementProtocol (SNMP), and others can also be implemented using substantiallyconventional software processes or modules executing on one or moremicroprocessors within exemplary IBRs. Such applications protocols canget access to or be accessed from any of the depicted network interfacesin FIGS. 31 and 32 via industry-standard Transmission Control Protocol(TCP) or User Datagram Protocol (UDP) transport layer protocols and theInternet Protocol (IP) network layer protocol. TCP, UDP and IP can beimplemented using substantially conventional software processes ormodules executing on one or more microprocessors within exemplary IBRs.Note that in certain deployments, such as backhaul within a cellularoperator's radio access network (RAN), messages to or from HTTP, SNMP orother applications protocols may need to be sent either via othertransport and network protocols or via encapsulation of TCP/UDP and IPsegments and packets within such other transport and network protocols(not shown in FIGS. 31 and 32). Note further that messages to or fromapplications protocols in the IBR may also bypass the TCP/UDP and IPprotocols, or their equivalents, entirely during a console mode (notshown) using a locally connected terminal.

FIGS. 31 and 32 also illustrate an exemplary element entitled “IBRControl” which is typically implemented as a distribution plane ofinterconnects, buses and/or controllers that arbitrate directcommunications between the RRC and RLC entities with various elements ofthe IBR MAC and IBR PHY. Because the IBR Control does not passinformation amongst such entities by using the communications protocolsstack, such information can be communicated with minimal latency forreal time control.

FIG. 33 illustrates an exemplary implementation of the IBR MAC 612. TheIBR MAC 612 is shown in terms of various functional elements and some oftheir relationships to each other as well as to the IBR PHY, the IBRLLC, the RRC, the RLC and the IBR Control. Operation of the IBR MAC ofFIG. 33 may depend on the type of “superframe” timing utilized.Typically, IBRs send a single PPDU per Modulator Core-j (or per transmitstream k), which may include Training Data blocks as described above, ina given transmit superframe (TxSF) and conversely will receive a singlePPDU per Demodulator Core-j (or per receive stream l) in a given receivesuperframe (RxSF).

As shown in FIG. 33, the IBR MAC 612 includes a IBR MAC managemententity 3304, a MAC Tx Buffer and Scheduler 3308, an IBR MAC ControlEntity 3312, a MAC Rx Buffer 3316, a decryption block 3320, anencryption block 3324, a MPDU header generator 3328, a first FCSgenerator 3332, a MPDU header analyzer 3336, a second FCS generator 3340and a FCS Pass? analyzer 3344.

FIG. 34 illustrates channel activity for a modulator and demodulatorpair j with data interface streams Tx-j and Rx-j respectively versustime for an exemplary IBR using FDD with fixed superframe timing.Similarly, FIG. 35 illustrates analogous channel activity for TDD withfixed superframe timing and FIG. 36 illustrates analogous channelactivity for TDD and Collision Sense Multiple Access (CSMA) withvariable superframe timing.

With reference back to FIG. 33, the operation of the IBR MAC is firstdescribed in the context of an example based on TDD/CSMA with variablesuperframe timing. As shown in FIG. 36, in CSMA transmissions by eitherthe AE-IBR or RE-IBR paired in an active link, whether PTP or PMP,defers to other channel activity detected within its present receiveantenna pattern. In practice, this can be achieved by using the receiveportion of the IBR PHY to determine in channel and in-view signal energywhich if above a threshold causes an inhibit control signal at either aTx PLCP Mod-j of FIG. 27 (not shown) corresponding to the affected linkor at the MAC Tx Buffer and Scheduler of FIG. 33 (not shown) identifyingthe affected link. For purposes of this description, the latter optionis considered. Furthermore, it is assumed that for this specific exampleevery MSDU or frame request at the MAC Tx Buffer and Scheduler resultsin a single MPDU based on such MSDU or frame request (see, for example,FIG. 4) that is then matched to a single PPDU in the Tx PLCPcorresponding to a given link. Other variants are possible with the IBRMAC and IBR PHY as discussed subsequently.

With reference again to FIG. 33, the primary source of MSDUs to the MACTx Buffer and Scheduler 3308 is typically in the data plane from the IBRLLC 3348. Either MSDUs and/or frame requests in the control plane canoriginate from the RRC 660 (or indirectly from the optional IBMS Agent700), the RLC 656, the IBR MAC Management Entity 3304, or the IBR MACControl Entity 3312. Exemplary details of frame requests and/or MSDUsoriginating from the RRC 660 or RLC 656 are discussed subsequently.

Exemplary frames originating at the IBR MAC Management Entity 3304include those associated with management processes such as Association,Authentication and Synchronization. In some cases, the IBR MACManagement Entity 3304 may send an MSDU payload to the MAC Tx Buffer andScheduler 3308 with a specific frame request type. In other cases, theIBR MAC Management Entity 3304 may send only the specific frame requesttype wherein all relevant information to be conveyed to the receivingIBR(s) will be present in the MPDU Header to be generated based on thedetails of the frame request type and other information presently knownto the IBR MAC.

In some embodiments, Association and Authentication processes can occurvia exchange of management frames in a substantially conventionalfashion. A particular RE-IBR may choose to associate with a given AE-IBRby sending an Association Request management frame directed to theAE-IBR based on either advertised information received from such AE-IBRand/or configuration information currently present in the RE-IBR. Uponreceipt of an Association Request, the AE-IBR can proceed according toits presently configured policies to associate with or deny associationto the RE-IBR. If associated, the AE and RE would exchangeauthentication frames in substantially conventional fashion to ensurethat compatible encryption/decryption keys are present for subsequentframe exchanges.

In exemplary IBRs, an RE-IBR can, for example, associate with adifferent AE-IBR if its present AE-IBR (or its wireline link interface)fails, the link throughput falls below a minimum threshold, the presentAE-IBR forces a disassociation, the present AE-IBR inhibits linkresource allocations to the RE-IBR below a minimum threshold, or theRE-IBR becomes aware of a preferred AE-IBR, all as set by certainconfiguration policies at the time as may be set by the optional IBMSAgent 700 as shown in FIG. 33. Furthermore, certain exemplary IBRs witha plurality of modulator cores can as an RE-IBR maintain a plurality ofcurrent associations with multiple AE-IBRs per configuration policies toenable enhanced throughput and/or link diversity.

Another set of exemplary management frames issued by the IBR MACManagement Entity 3304 concerns synchronization, status and presence.Periodically, (as configured or directed by the optional IBMS Agent 700)an exemplary AE-IBR may choose to send a Synchronization Frame thatadvertises certain capabilities of the AE-IBR including wireline linkfailure conditions and provides a time stamp reference usable byexemplary RE-IBRs for timing synchronization as either broadcastuniformly across the full directionality possible for the IBR AntennaArray and/or across all current links. Advantageously, particularly foran AE-IBR with multiple associated RE-IBRs in a PMP configuration, sucha Synchronization Frame (or other such management frame) can direct oneor more RE-IBRs to make internal reference timing offsets such that thetime of arrival of transmissions from such RE-IBRs is more optimallyaligned for best simultaneous reception at the AE-IBR in either FDD orTDD with fixed superframe timing (see FIGS. 34 and 35). For example, theAE-IBR may determine such timing offsets within theAcquisition/Synchronization element of the IBR Channel MUX 628 byanalyzing preamble samples corresponding to particular RE-IBRtransmissions.

With reference again to FIG. 33, exemplary frames originating at the IBRMAC Control Entity 3312 include those associated with control processessuch as Acknowledgement and Access Control. Analogously to the IBR MACManagement Entity 3304, the IBR MAC Control Entity 3312 may send an MSDUpayload to the MAC Tx Buffer and Scheduler 3308 and/or a specific framerequest type wherein relevant information can be conveyed to thereceiving IBR in the MPDU Header.

In exemplary IBRs, Acknowledgement Frames can provide an ACK or NACKindication for configured frame types recently received. The frames areidentified uniquely and then set to ACK or NACK based on the receivepath FCS comparison process illustrated in FIG. 33. To minimizetransport overhead, implementation complexity and transmit latency, someembodiments of the IBR utilize a NACK protocol administered by the IBRMAC Control Entity. With reference to FIGS. 34-36, upon receipt of oneor more MPDUs within RxSF(s), where “s” is a superframe sequence number,then if any MPDU has an FCS failure within RxSF(s), a NACK bit is set inthe MPDU Header of the first (or each) MPDU within TxSF(s+1). If theoriginating IBR detects a positive NACK in TxSF(s+1) at its receiver,then such an IBR will re-transmit via its MAC Tx Buffer and Scheduler3308 the MPDU (or MPDUs) associated with RxSF(s) using link parametersas determined by its RLC 656 at that time. For the FDD case of FIG. 34,such re-transmitted MPDU (or MPDUs) originally from RxSF(s) would atleast partially be received in RxSF(s+2) whereas for the TDD cases ofFIGS. 35 and 36, it would be RxSF(s+1). If there were no FCS failures inRxSF(s), or the originating IBR fails to detect a positive NACK inTxSF(s+1) for any reason, then the originating IBR will clear the MPDU(or MPDUs) associated with RxSF(s) from its MAC Tx Buffer and Scheduler3308. Note that unlike conventional ACK protocols, this exemplary IBRNACK protocol does not guarantee 100% delivery of MPDU. However,occasional MPDU delivery failures are typically correctable at a higherlayer for data plane MSDUs (i.e., using TCP or an equivalent transportlayer protocol), non-catastrophic for management or control plane framesto the IBR MAC Management Entity 3304, the IBR MAC Control Entity 3312,the RRC 660, or the RLC 656, and preferable to the increased latency andjitter of conventional ACK protocols applied to backhaul for those dataplane MSDUs not subject to higher layer correction (i.e. using UDP or anequivalent transport layer protocol). Note further that this NACKprotocol is also advantageously used when PLCP Header FCS failures occurby, for example, having the Rx PLCP Demod-j discarding such a failedPPDU but substituting an MPDU with correct link ID but dummy FCS toRxD-j in FIGS. 29 and 30 to trigger an FCS failure at the IBR MAC 612.

In some embodiments, Access Control Frames are initiated at the IBR MACControl Entity 3312 to control the behavior of other IBRs with currentlinks to the initiating IBR. Such Access Control Frames can, forexample, restrict the rate at which data plane MSDUs are sent, restrictthe timing in which data plane MSDUs are sent, or temporarily inhibitfurther data plane MSDUs from being sent in a local overloadingscenario. For example, an exemplary AE-IBR could utilize Access ControlFrames to enforce access policies discriminatorily amongst multipleRE-IBRs according to certain configuration parameters such as a ServiceLevel Agreement (SLA). Such access policies may also be set via theoptional IBMS Agent 700 as shown in FIG. 33.

With reference to FIG. 33, the MAC Tx Buffer and Scheduler 3308temporarily stores data plane MSDUs from the IBR LLC 3348 as well asframes or frame requests from the IBR MAC Management Entity 3304, IBRMAC Control Entity 3308, RRC 660 and/or RLC 656 until such data can bescheduled for transmission within one or more MPDUs. Such scheduling isadvantageously performed based on policies either configured locally oroptionally communicated from the IBMS Agent 700 via the RRC 660 and theIBR Control 3352. In some embodiments, data plane MSDUs from the IBR LLC3348 usually are the lowest priority in the queue for schedulingcomposition of the next MPDU. If the rate of MSDU delivery from the IBRLLC 3348 exceeds the instant link delivery capability, then to avoidbuffer overflow the MAC Tx Buffer and Scheduler 3308 may have an Xon/offcontrol feedback to the IBR LLC 3348 to cause the IBR LLC 3348 to stopsending MSDUs until the appropriate buffer status returns. This mayresult in the IBR LLC 3348 causing certain other interfaces such as anEthernet or WiFi interface to reduce MSDU traffic. To the extent thatthe ratio of control plane traffic to data plane traffic is small, as isby design for some embodiments, then scheduling priority amongst framesother than MSDUs from the IBR LLC 3348 is unimportant and “first-in,first-out” is sufficient.

Note that the foregoing embodiment of the MAC Tx Buffer and Scheduler3308 performs scheduling based on frame type without regard for otherinformation such as the PCP within an 802.1 MAC frame as may be presentin MSDUs from the IBR LLC 3348. The IBR LLC 3348 in its bridgingcapacity may forward MSDUs to the MAC Tx Buffer and Scheduler 3308 inorder based on PCP (or other such QoS or CoS indicators) so that the MACTx Buffer and Scheduler 3308 need not repeat the queuing exercise. Inalternative embodiments, such QoS prioritization of MSDUs can also beperformed at the MAC Tx Buffer and Scheduler 3308 instead.

Upon scheduling an MPDU for transmission as described above, the MAC TxBuffer and Scheduler 3308 causes the MPDU Header Generator 3328 tocompose an MPDU Header specific to the pending MPDU. In conventionalIEEE 802 based communications systems, such an MPDU Header would includeat least the physical address (also known as the “MAC address” or the“hardware address”) of both the origination and destination IBRs.However, sending such physical addresses (typically 48 or, morerecently, 64 bits) in every MPDU unduly burdens the IBR links withunnecessary overhead that reduces MAC efficiency. Thus, in someembodiments, a Link Identifier (LID) is substituted in every MPDU headerinstead. Exemplary LID implementations can be as few as 16 bits inlength. For example, each exemplary LID may include an AE-IBR identifierof 10 bits and an identifier of 6 bits for an RE-IBR presentlyassociated with the AE-IBR. This is possible because in some embodimentsthe IBRs are configured in view of their fixed geographic positions inthe field as set at time of deployment or optionally controlled by theIBMS Agent 700 such that no overlapping AE-IBR identifiers are withinradio range of RE-IBRs possibly associated with them. The AE-IBR mayassign a locally unique RE-IBR association identifier field as part ofthe association process. For unassigned links, all zeros (or ones) canbe sent for LID and then the frame payload, for example a managementframe used in the association process, can include the full physicaladdresses as appropriate. Note that even if, in the alternative, thatlonger (possibly 24 bits or 32 bits) “regionally-unique” or even“globally-unique” LIDs were used, then because the overall number ofworldwide backhaul links is generally much less the overall number ofworldwide network devices, such extended length LIDs can still be muchshorter than traditional IEEE 802 based addressing schemes.

A Frame Type Identifier (FTI) may be placed in the MPDU header by theMPDU Header Generator 3328. In one embodiment, the FTI is no more than 5bits total. In one particular embodiment, the FTI is part of a FrameControl Field (FCF) of 8 bits, and the other 3 bits include 1 bit forthe NACK protocol control bit indicator (set to 1 if the previousRxSF(s) had an MPDU with an FCS failure), 1 bit to indicate if theinstant frame of the MPDU payload is encrypted, and 1 bit to indicate ifthe instant frame of the MPDU payload is the last frame (LF) in thepayload. Alternatively, the 1 bit for the NACK can be 1 bit for the ACKindicator (set to 1 if the previous RxSF(s) had an MPDU without an FCSfailure) if an ACK protocol is used for the instant MPDU FTI. Followingthis FCF byte, a 16 bit Fragment and Length Indicator (FLI) is placedsequentially in the MPDU header, wherein, for example, 3 bits of the FLIindicates by 1 bit if the instant frame payload is the last fragment andby 2 bits the fragment sequence number and 13 bits indicate the instantframe payload length in bytes. Following the 2 FLI bytes, an 8 bit FrameSequence Number (FSN) is placed sequentially in the MPDU header. The FSNare typically sequentially generated except where repeated for thoseframe payloads sent as fragments. If LF=1 in the initial FCF byte of theMPDU header (as would be the case for the single MSDU of frame payloadper MPDU scenario described above for TDD/CSMA), then the MPDU header iscomplete. If the MAC Tx Buffer and Scheduler 3308 is configured topermit concatenation of MSDUs or other frame payloads up to some maximumMPDU payload (as would be compatible with many TDD/CSMA deployments),then LF=0 when FLI describes an instant frame payload lengthsufficiently low to allow another available frame payload to beconcatenated within the maximum MPDU payload length and an additionalFCF, FLI and FSN combination would be generated at the MPDU HeaderGenerator 3328 and repeated until an FCF with LF=1 is encountered. Notethis process of concatenated FCF, FLI and FSN fields within an MPDUheader corresponding to concatenated frame payload can also beadvantageously applied to fixed superframe timing in either FDD or TDDas illustrated in FIGS. 34 and 35.

The MAC Tx Buffer and Scheduler 3308 further provides the one or moreframe payloads that form the MPDU payload to the Encryption element 3324to be encrypted on a frame payload by frame payload basis as indicatedin the FCF using substantially conventional encryption algorithms. Anexemplary algorithm suitable for the IBR is the Advanced EncryptionStandard (AES) which has been published by the National Institute ofStandards and Technology. In one embodiment, the IBRs use AES with a 256bit key length. Other key lengths and other encryption algorithms arealso possible for exemplary IBRs. Exemplary IBRs can also employencryption for all frames after encryption keys are exchanged duringauthentication (and even including association and authentication framesto the extent encryption keys sufficient at least for association andauthentication are provided to IBRs via, for example, factory setting orconsole mode interface).

The encrypted (and/or unencrypted as desired) frame payload(s) and theMPDU header are then concatenated together as shown in FIG. 33 and thenpassed through an FCS Generator 3332 that generates an FCS (e.g., of atleast 32 bits in length). Alternatively, some IBR embodiments may alsoencrypt (and decrypt) MPDU headers. Other IBR embodiments may attainsome measure of MPDU header privacy (and PLCP header privacy) by settingscrambler and descrambler parameters (see FIGS. 19-22) derived from, forexample, the encryption keys and/or LID. The FCS is then appendedfollowing the MPDU header and frame payload(s) as also shown in FIG. 33to complete the composition of an MPDU to be sent to the IBR PHY 3356over the Tx Data interface.

Note also that for those frame types, particularly certain managementframes originating at the AE-IBR of a PMP configured deployment, thatare intended to be broadcast to all current links at an IBR, such framepayloads may be distributed to all such links in parallel at the MAC TxBuffer and Scheduler 3312 such that the same frame payload is providedto at least one MPDU corresponding to each current link. The IBRstypically generate very little broadcast traffic and most Ethernet orWiFi broadcast traffic on the other IBR interfaces is filtered at theIBR LLC 3348.

With reference to FIG. 33, the receive path of the exemplary IBR MACperforms essentially the reverse operations described above in thetransmit path. Starting with the IBR PHY 3356, after the Rx PLCPanalyzer 1808 (see FIG. 18) recovers an MPDU, it is passed via the RxData interface in FIG. 33 to a splitter 3360 within the IBR MAC. Thesplitter 3360 removes the trailing bits of the MPDU corresponding to theFCS, or RxFCS. The remainder of the MPDU minus RxFCS is passed throughan FCS

Generator 3340, the result of which is compared at FCS Pass? analyzer3344 to determine if it is identical to RxFCS. If it is identical, thena known-good (barring the extraordinarily rare false positive FCS event)MPDU is received. The FCS Pass? status is communicated to the IBR MACControl Entity 3312, the MAC Rx Buffer 3316, the MPDU Header Analyzer3336, and the RRC 660 and RLC 656 (for analytical purposes) as shown inFIG. 33. The MPDU Header Analyzer 3336 receives from a second splitterthe leading bits of the MPDU corresponding to a minimum length MPDUheader described above. If LF=1, then the remaining payload portion ofthe MPDU is passed to the Decryption element 3320 (or bypassed ifappropriate) for decryption when the encryption indicator bit of the FCFis set. The MPDU Header Analyzer 3336 may also verify (or cause to beverified) that the payload length corresponds to that described in theFLI field of the MPDU Header and that the LID is valid. Upon decryption(as appropriate), the MPDU payload is passed to the MAC Rx Buffer 3316which then forwards the MSDU or frame payload to the IBR MAC ManagementEntity 3304, the IBR MAC Control Entity 3312, the IBR LLC 3348, the RRC660 or the RLC 656 as appropriately directed by the MPDU Header Analyzer3336 based on LID and FTI. The MPDU Header Analyzer 3336 may alsodirectly signal the IBR MAC Control Entity 3312 with the status of theNACK bit in the exemplary MPDU header described above. In the event thatthe instant frame payload is a fragment, as evident by the FLI field inthe exemplary MPDU header described above, then the MPDU Header Analyzer3336 instructs the MAC Rx Buffer 3316 based on the FSN field to eitherstore the fragment, concatenate the fragment to one or more other storedfragments, or deliver the multiple fragments if the instant fragment hasthe last fragment indicator within the FLI field as described above.Optionally if a positive ACK protocol is used for 100% delivery of everyMPDU (versus the superframe NACK protocol described above), then theMDPU Header Analyzer 3336 also verifies the FSN for duplicated detectionand discards (or causes to be discarded) such duplicate payloads.

In the event that the MPDU being received has multiple concatenatedMSDUs and/or frame payloads as described optionally above, then the MPDUHeader Analyzer 3336 interacts with the second splitter via the feedbacksignal shown to continue parsing off consecutive MDPU header bytes, forexample the repeated exemplary FCF, FLI and FSN fields, until an FCFwith LF=1 is encountered. The above described process for the MPDUHeader Analyzer 3336 directing the Decryption element 3320 and the MACRx Buffer 3316 to deliver the multiple payloads is then repeated eitherserially or in parallel as desired until all contents of the MPDUpayload have been resolved by the IBR MAC.

In the event that the FCS Pass? analyzer 3344 described above determinesan FCS failure then the receive path of the exemplary IBR MAC operatesdifferently depending on certain options that may be designed into theIBR or selected based on configuration policies. For the superframe NACKprotocol described above, the FCS failure is directly communicated tothe RRC 660 and RLC 656 (via the IBR Control 3352 of FIGS. 31-33) fortheir analytical purposes and is directly communicated to the IBR MACControl Entity 3312 so that TxSF(s+1) is sent with NACK=1 in theexemplary MPDU header described above. Optionally, the MPDU HeaderAnalyzer 3336 may attempt to determine if an apparently valid MPDUheader is present, and, if so, attempt to deliver certain MSDUs or framepayloads as described above for the case of a known-good MPDU. However,as directed by configuration policies, certain frame types may bediscarded. For example, in one embodiment, only MSDUs to the IBR LLC3348 that correspond to apparently valid MPDU header fields would bedelivered in an FCS failure situation, and even then only afterbuffering such MSDUs for one additional superframe period to determineif a duplicate FSN MSDU may be available due to the re-transmissionattempt associated with the superframe NACK protocol described above.Alternatively, in the case of an ACK protocol that guarantees 100%delivery of known-good MPDUs, then the entire MPDU payload is discarded.

For the types of data throughput rates and superframe lengths that arepractical, the single payload MPDU per superframe example describedabove for the TDD/CSMA example of FIG. 36 is not an optimum choice forthe fixed superframe timing examples for FDD in FIG. 34 or TDD in FIG.35. One alternative uses concatenated multi-payload frame MPDUs up tosome maximum length and then forwards such MPDUs to the Tx PLCP tocompose PPDUs as described previously. Another alternative, compatiblewith the superframe NACK protocol described above, would have the MAC TxBuffer and Scheduler 3308 utilize the same information from the RLC 656and the RRC 660 available to the Tx PLCP and thus compose a singlemulti-payload MPDU that will, with appropriate padding added in the TxPLCP to an integer block count, maximally occupy the available PPDU forthe pending superframe.

Note that for the TDD case depicted in FIG. 35 with fixed superframetiming, IBRs are capable of operating in such modes wherein thesuperframe timing in the forward link from AE to RE may be differentthan in the reverse link. For a PMP AE-IBR this typically requires thatall RE-IBRs adopt the same superframe timing parameters in associationwith this particular AE-IBR. Some RE-IBRs, in either PTP or PMPconfigurations, may be simultaneously associated with two or moreAE-IBRs to the extent such IBRs permit this policy and have sufficientradio resources to maintain such links. Given that multiple AE-IBRsassociated with such RE-IBRs can adopt different TDD fixed superframetiming parameters relative to each other, such timing parameters may becommunicated to all RE-IBRs via management frames originating in the IBRMAC Management Entity 3304. Similarly, to the extent an RE-IBR islimited in superframe timing access due to such multiple associations,such an RE-IBR can communicate such restrictions to the AE-IBRs viamanagement frames from its IBR MAC Management Entity 3304.

For PMP configurations, the AE-IBR can advantageously transmit to orreceive from multiple RE-IBRs simultaneously in a given radio channelusing SDMA as described above. To the extent that the number of RE-IBRsassociated with an AE-IBR exceeds either the AE-IBR's available SDMAresources or certain RE-IBRs are not spatially separable by the AE-IBR,then simultaneous transmissions to such RE-IBRs would require multipleradio channels which in practice is often either undesirable orimpractical. Another alternative for maintaining links to RE-IBRswherein such SDMA capabilities are being exceeded is through the use ofTime-Division Multiplexing (TDM). For either an FDD or TDD system withfixed superframe timing, such as depicted in FIGS. 34 and 35, an AE-IBRcan use TDM to designate certain “subframes” within a given superframeapplied to a modulator/demodulator resource pair j to particular LIDs.Management frames from the AE-IBR's IBR MAC Management Entity 3304 can,in exemplary embodiments, inform affected RE-IBRs of such LID to TDMsub-frame mappings and associated subframe timing parameters. In someembodiments, any RE-IBR associated with two or more AE-IBRssimultaneously could request that such LID to TDM sub-frame mappingsand/or timing parameters account for its local timing preferences foroptimally maintaining such simultaneous links. The MAC Tx Buffer andScheduler 3308 may compose MPDUs in view of TDM sub-frame timingparameters that are assigned such that the TxPLCP can optimally utilizean integer number of transmit blocks in each sub-frame. The number ofsub-frames per superframe are typically relatively low (e.g., usuallyless than 5).

To the extent that IBRs deployed in the field are within co-channelinterference range of each other and configured to use overlappingchannels in general or periodically, such IBRs advantageouslysynchronize their TDD fixed superframe timing to minimize simultaneousco-channel TxSF/RxSF overlaps amongst disparate links. Several exemplarysynchronization strategies may be used by such IBRs to align superframetiming boundaries in such scenarios. For example, if “free-running” or“self-synchronizing” IBRs are able to detect at least a preamble, atraining block, a PLCP header, an unencrypted MPDU header, or otherinformation such as management frames with timing information that maybe decipherable without link-specific encryption keys that correspond tolinks involving a different AE-IBR, then the slower in time IBRs mayadopt the superframe timing boundary and cadence of the faster in timeIBRs. At the AE-IBR, which may act as a local timing master, this can beperformed directly by making a timing offset and communicating it to isassociated RE-IBR(s). At the RE-IBR, which may be able to detectdisparate link information otherwise undetectable at its associatedAE-IBR, the RE-IBR can inform its AE-IBR via a management frame of anytiming offset necessary to obtain local disparate AE-IBR co-channelsuperframe timing synchronization. It will be appreciated that thisprocess is ongoing because after synchronizing, the reference clocks inthe AE-IBRs inevitably will drift differently over time.

In certain field deployment scenarios, IBRs located in the same regionalarea may be capable of undesirably interfering with each other at rangesbeyond their ability to detect and synchronize as described above. Analternative synchronization strategy better suited to this situationwould utilize a network-wide central synchronization capability. Oneexample of this would be the use of Global Positioning Satellite (GPS)timing at each AE-IBR. GPS is more than adequate in terms of timingaccuracy for the needs of synchronizing superframe timing boundaries.However, GPS adds cost, size, power consumption and form factorconstraints that may be undesirable or unacceptable to some IBRs. Notefurther that because IBRs are designed to operate in street leveldeployments with obstructed LOS, GPS may fail to operate in places whereRE-IBRs function normally. Another alternative would be to use asystem-wide synchronization technique such as SynchE or IEEE 1588v2. Inthis scenario, AE-IBRs are configured to derive timing parameters in aconsistent fashion. Alternatively, the AE-IBRS include IBMS Agentscapable of coordinating such configurations when co-channel operation ina mutual interfering deployment is encountered.

In the deployment scenario where multiple AE-IBRs are co-located (e.g.,at a single pole, tower, building side or rooftop), even if such IBRsare configured to avoid co-channel operation, at least some form oflocal superframe timing synchronization for TDD may be utilized to avoidoverloading receiver RF/analog circuits from simultaneous in-bandtransmissions and receptions amongst the co-located IBRs. One exemplarystrategy for the above synchronization would be to distribute by hardwiring a local superframe timing synchronization signal which can beconfigured at or arbitrarily assigned to any one of the co-located IBRs.

Note that the foregoing descriptions and figures for exemplary IBRembodiments have provided minimal internal details on the distributionof various clocks and timing references amongst the structural andfunctional elements of the IBR. These exemplary embodiments can all berealized using substantially conventional strategies for internal timingdistribution.

As described above, IBRs with fixed superframe timing may use a NACKprotocol wherein a previous superframe FCS failure in receive causesNACK=1 in an MPDU header of the respective link in transmitting its nextsequential superframe PPDU back to the sender of the MPDU received inerror. If the original sender detects NACK=1, then a re-transmission ofthe previous superframe PPDU contents occurs at the direction of its MACTx Buffer and Scheduler 3308. Otherwise, the original sender discardsthe previous superframe PPDU contents at its MAC Tx Buffer and Scheduler3308. This approach is different from many conventional wireless datanetworking protocols that use ACK receipt to guarantee 100% delivery atthe MAC layer even if theoretically unbounded re-try attempts may berequired. This fixed superframe NACK protocol is similar to using an ACKprotocol with a “time to live” of effectively one superframe durationafter initial transmission. This approach advantageously bounds thelatency at a very low length for processing frames through the IBR MACwithout resorting to reliability of simply the raw frame error rate. Byallowing one immediate re-transmission opportunity, this fixedsuperframe NACK protocol effectively produces a net frame error ratethat is the square of the raw frame error rate. For example, if the rawframe error rate were 10⁻³ (1 in 1000), the net frame error rate per thefixed superframe NACK protocol should be approximately 10⁻⁶ (1 in1,000,000).

To improve the reliability of the fixed superframe timing NACK protocoleven further, IBRs may have the TxPLCP set a 1 bit field in the PLCPheader(s) for the Modulator Core j corresponding to the LID with NACK=1(or with a previous RxSF(s) PLCP header FCS failure as described above).This approach advantageously exploits the fact that PLCP headers,typically sent at the most reliable MCS, are of short duration andalways sent immediately after the Training Block 0 (see FIG. 26) wherethe channel equalization coefficients most accurately reflect currentconditions. Thus, a NACK bit sent in a PLCP header is likely to bereceived accurately even if the PPDU payload that includes the MPDUheader NACK field is not. In the case where NACK=1 in a PLCP header, anexemplary PLCP Header Analyzer 3004 (see FIG. 30) will signal theexemplary MAC Tx Buffer and Scheduler 3308 via the IBR Control 3352. Inthe case where an originator of an MPDU does not receive a valid NACKfield in either the PLCP header or the next MPDU header of a subsequenttransmit superframe, then the MAC Tx Buffer and Scheduler 3308 maychoose to re-send the pending MPDU(s), possibly at a more reliable MCSas directed by the RLC 656, or may choose to discard the pending MPDU(s)so as not to cascade latency for further frames awaiting transmission.Such a decision may be made based on configurable policies that may varywith current conditions or be updated by the IBMS Agent 700. To theextent that a “blind” retransmission is made due to an invalid NACKfield wherein the actual NACK field value was NACK=0, then the receivepath MPDU Header Analyzer 3336 at the destination IBR will discard there-sent MPDU(s) based on duplicate detection of the FSN at the MPDUHeader Analyzer 3336 shown in FIG. 33. The MPDU Header Analyzer 3336 mayalso report incidents of duplicate detections of MPDUs for a given LIDto the RRC 660 and RLC 656 as shown in FIG. 33. This provides anadvantageous additional local indication to the RRC 660 and RLC 656 ofproblems being encountered in the transmit direction from such an IBRfor the particular LID.

With reference to FIGS. 31 and 32, the RRC 660 and RLC 656 interact withthe IBR MAC 612 and various elements of the IBR PHY both via “normal”frame transfers and direct control signals via the conceptual IBRControl plane. Both the RRC 660 and the RLC 656 may execute concurrentcontrol loops with the respective goals of optimizing radio resourceallocations and optimizing radio link parameters for current resourcesin view of the dynamic propagation environment conditions, IBR loading,and possibly system-wide performance goals (via the optional IBMS Agent700). It is instructive to view the RLC 656 as an “inner loop”optimizing performance to current policies and radio resourceallocations for each active link and to view the RRC 660 as an “outerloop” determining if different policies or radio resource allocationsare desirable to meet overall performance goals for all IBRs currentlyinteracting with each other (intentionally or otherwise). Typically boththe RRC 660 and the RLC 656 are implemented as software modulesexecuting on one or more processors.

The primary responsibility of the RLC 656 in exemplary IBRs is to set orcause to be set the current transmit MCS and output power for eachactive link. In one exemplary embodiment described above, the RLC 656provides information to the TxPLCP that enables, for example, a PLCPController 2812 in FIG. 28 to set the MCS for a particular LID. Inanother embodiment compatible with the single MPDU for fixed superframetiming with NACK protocol example of IBR MAC operation, the RLC 656determines the MCS for each LID and then communicates it directly to theMAC Tx Buffer and Scheduler 3308 of FIG. 33 and the PLCP Controller 2812for every TxPLCP Mod-j of FIGS. 27 and 28. The RLC 656 causes thetransmit power of the IBR to be controlled both in a relative senseamongst active links, particularly of interest for the AE-IBR in a PMPconfiguration, and also in an overall sense across all transmits chainsand antennas. In an exemplary IBR embodiment, the RLC 656 can cause suchtransmit power control (TPC) as described above by setting parameters atthe Channel Equalizer Coefficients Generator 2332 of FIG. 23 (forrelative power of different simultaneous modulation streams), at eachactive transmit RF chain Tx-m 636 of FIGS. 6, 7 and 16 (for relativepower of different simultaneous RF chains) and at each Front-end PA1104, 1204 within the IBR Antenna Array of FIGS. 6, 7, 10-12 (for totalpower from all antennas).

In some embodiments, the RLC 656 can determine its MCS and TPCselections across active links based on information from various sourceswithin the IBR. For example, the IBR MAC can deliver RLC control framesfrom other IBRs with information from such other IBRs (for example,RSSI, decoder metrics, FCS failure rates, etc.) that is useful insetting MCS and TPC at the transmitting IBR. Additionally, such RLCcontrol frames from an associated IBR may directly request or demandthat the RLC in the instant IBR change its MCS and/or TPC values fortransmit directly on either a relative or absolute basis. For TDD IBRdeployments, symmetry of the propagation environment (in the absence ofinterference from devices other than associated IBRs) makes receiverinformation useful not only for sending RLC control frames to thetransmitting IBR but also for use within the receiving IBR to set itstransmitter MCS and/or TPC. For example, the FCS Pass? analyzer 3344 andMPDU Header Analyzer 3336 of the exemplary IBR MAC in FIG. 33 can supplythe RLC 656 with useful information such as FCS failures, duplicatedetections and ACK or NACK field values. Similarly, each PLCP HeaderAnalyzer 3004 as shown in FIG. 30 can send the RLC FCS failure status onthe PLCP Header and/or PPDU payload(s). Another possibility is to havethe PLCP Header carry a closed-loop TPC control field requesting a TPCstep up or down or stay the same. Additionally, the Channel EqualizerCoefficients Generator 2332 in computing channel weights can provide SNRand/or SINR information per demodulator stream that can help the RLC setMCS and/or TPC as shown in FIG. 23. Each decoder within each demodulatorcore j can provide the RLC 656 with decoder metrics useful for MCSand/or TPC as indicated by FIGS. 20 and 22 for example. And each receivechain Rx-n 640 of FIG. 17 can provide receive signal strength indicator(RSSI) values helpful especially for determining TPC requests back tothe transmitting IBR.

The actual MCS values are typically selected from a finite length listof modulation types and coding rates. Exemplary IBRs can use QAM rangingfrom 2-QAM (better known as BPSK), through 4-QAM (better known as QPSK),16-QAM, 64-QAM, 256-QAM and 1024-QAM. Exemplary IBRs can use a basecoding rate of ⅓ or ½ and then can use “puncturing” (whereinpredetermined bit positions are deleted in transmit and replaced bydummy bits in receive) to derive a set of effective coding rates of, forexample only, ½, ⅔, ¾, ⅚, ⅞, and 9/10. In typical embodiments, thelowest MCS index corresponds to the lowest available QAM constellationsize and the lowest available coding rate (i.e. the most reliabletransmission mode) and the highest MCS index corresponds to theconverse.

The TPC absolute range tends to be lower for IBRs than that desired formany conventional wireless networking systems operating in obstructedLOS due to the more limited range of separations between AE-IBRs andRE-IBRs for backhaul applications (i.e. backhaul radios are almost neverplaced in close proximity to each other). The relative variation indesired power between active links at an AE-IBR may also limited inrange particularly by the transmit DACs.

Many possible algorithms are known for generally relating informationprovided to the RLC 656 as described above to selecting MCS and TPCvalues. In dynamic propagation environments, averaging or dampeningeffects between channel quality information and MCS changes areadvantageously utilized to avoid unnecessarily frequent shifts in MCS.To the extent that an IBR is operating at below the maximum allowableTPC value, it is generally advantageous to permit TPC to vary morequickly from superframe to superframe than the MCS. However, ifoperating at maximum allowable TPC, then it is often advisable toimmediately down select MCS to a more reliable setting upon detection ofan MPDU FCS failure and/or a NACK=1 condition. Conversely, up selectingMCS is usually performed only after repeated superframe metricsindicating a high likelihood of supporting an MCS index increase. At thelimit, where RLC 656 has reached maximum TPC and minimum MCS (mostreliable mode), to maintain ongoing link reliability, the imperativeincreases for the RRC 660 to allocate different resources to enable theRLC 656 to operate again in MCS and TPC ranges with margin for temporalchannel impairment.

The primary responsibility of the RRC 660 is to set or cause to be setat least the one or more active RF carrier frequencies, the one or moreactive channel bandwidths, the choice of transmit and receive channelequalization and multiplexing strategies, the configuration andassignment of one or more modulated streams amongst one of moremodulator cores, the number of active transmit and receive RF chains,and the selection of certain antenna elements and their mappings to thevarious RF chains. Optionally, the RRC may also set or cause to be setthe superframe timing, the cyclic prefix length, and/or the criteria bywhich blocks of Training Pilots are inserted. The RRC 660 allocatesportions of the IBR operational resources, including time multiplexingof currently selected resources, to the task of testing certain linksbetween an AE-IBR and one or more RE-IBRs. The RRC 660 evaluates suchtests by monitoring at least the same link quality metrics as used bythe RLC 656 as evident in the exemplary embodiments depicted in FIGS. 6,7, 17, 18, 20, 22, 23, 29, 30, 31, 32 and 33. Additionally, in someembodiments, additional RRC-specific link testing metrics such as thoseproduced by the exemplary Training Data Analyzer described above forFIG. 30 in relation to the exemplary Training Data Library of FIG. 28are used. The RRC 660 can also exchange control frames with a peer RRCat the other end of an instant link to, for example, provide certainlink testing metrics or request or direct the peer RRC to obtain linkspecific testing metrics at the other end of the instant link forcommunication back to RRC 660.

In some embodiments, the RRC 660 causes changes to current resourceassignments in response to tested alternatives based on policies thatare configured in the IBR and/or set by the optional IBMS Agent 700 asdepicted for example in FIGS. 7, 32, and 33. An exemplary policyincludes selecting resources based on link quality metrics predicted toallow the highest throughput MCS settings at lowest TPC value.Additional exemplary policies may factor in minimizing interference bythe instant link to other AE-IBR to RE-IBR links (or other radio channelusers such as conventional PTP radios) either detected at the instantIBRs or known to exist at certain physical locations nearby as set inconfiguration tables or communicated by the optional IBMS Agent 700.Such policies may also be weighted proportionately to reach a blendedoptimum choice amongst policy goals or ranked sequentially inimportance. Also as discussed above regarding the RLC 656, the RRC 660may have policies regarding the fraction of IBR resources to be used forRRC test purposes (as opposed to actual IBR backhaul operations) thatfactor the current RLC settings or trajectory of settings.

The RRC 660 in one IBR can communicate with the RRC in its counterpartIBR for a particular link AE-IBR to RE-IBR combination. For example, theRRC 660 sends RRC control frames as discussed for the exemplary IBR MACof FIG. 33 or invokes a training mode within the exemplary Tx PLCP asdiscussed for FIG. 28.

In some embodiments, for either PTP or PMP deployment configurations,the selection of either the one or more active RF carrier frequenciesused by the RF chains of the IBR RF, the one or more active channelbandwidths used by the IBR MAC, IBR Modem, IBR Channel MUX and IBR RF,the superframe timing, the cyclic prefix length, or the insertion policyfor blocks of Training Pilots is determined at the AE-IBR for any givenlink. The RE-IBR in such an arrangement can request, for example, an RFcarrier frequency or channel bandwidth change by the AE-IBR by sendingan RRC control frame in response to current link conditions at theRE-IBR and its current RRC policies. Whether in response to such arequest from the RE-IBR or due to its own view of current linkconditions and its own RRC policies, an AE-IBR sends the affectedRE-IBRs an RRC control frame specifying at least the parameters for thenew RF frequency and/or channel bandwidth of the affected links as wellas a proposed time, such as a certain superframe sequence index, atwhich the change-over will occur (or alternatively, denies the request).The AE-IBR then makes the specified change after receiving confirmationRRC control frames from the affected RE-IBRs or sends a cancellation RRCcontrol frame if such confirmations are not received before thescheduled change. In some deployment situations, the RRC policycondition causing the change in the RF carrier frequency and/or channelbandwidth for a particular LID may be a directive from the IBMS Agent700.

The selection of other enumerated resources listed above at an IBR cangenerally be made at any time by any given IBR of a link. Additionally,requests from the opposite IBR can also be made at any time via RRCcontrol frames. An RE-IBR typically attempts to utilize all availablemodulator and demodulator cores and streams as well as all available RFchains to maximize the robustness of its link to a particular AE-IBR. Inan RE-IBR embodiment where at least some redundancy in antenna elementsamongst space, directionality, orientation, polarization and/or RF chainmapping is desirable, the primary local RRC decision is then to chooseamongst these various antenna options. An exemplary strategy forselecting antenna options (or other enumerated resources listedpreviously) at the RE-IBR is to apply alternative selections of suchresources to the Training Data portion of PPDUs described above inrelation to the Tx PLCP and FIGS. 27 and 28. The RRC 660 at the RE-IBRthen compares link quality metrics such as those used by the RLC 656 andtraining data metrics from the exemplary Training Data Analyzer of FIG.30 to determine if the alternatively-selected resources are likely toresult in improved performance based on current IBR RRC policiescompared to the known performance of the currently-selected resources ofthe instant link. If the RRC 660, based on one or more such alternativeselection tests, decides that the instant link's performance goals arelikely to improve by using the alternately-selected resources, then theRRC 660 at such RE-IBR can cause such selections to become the newcurrent settings at any time and without requiring notification to theAE-IBR.

For the RE-IBR alternate resource selection process described aboveapplied to a TDD configuration, channel propagation symmetry for a givenlink (if interference is ignored) may make changing to a correspondingset of resources for transmit from such RE-IBR as have beenalternatively-selected for receive preferable. However, this isgenerally not true for an FDD configuration or a scenario where unknowninterference represents a significant channel impairment or where a PMPAE-IBR has simultaneous links to other RE-IBRs. In such scenarios, anRE-IBR may notify the AE-IBR when such RE-IBR is testingalternately-selected resources in a portion of its Tx PPDUs, whether inresponse to an RRC control frame request by the AE-IBR or by suchRE-IBR's own initiative, and then receive a return RRC control framefrom the AE-IBR that either reports the measured link quality metricsobserved at the AE-IBR and/or directs the RE-IBR to adopt thealternatively-selected resources for future Tx PPDUs from the RE-IBR onsuch link.

For the PTP configuration, an AE-IBR performs its RRC-directed alternateresource selections using substantially the same processes describedabove for the RE-IBR but with the roles reversed appropriately. In thePMP configuration, an AE-IBR may utilize similar RRC-directed testing ofalternate resource selections across its multiple current links but tothe extent that such links depend concurrently on certain resources, thedecision to actually change to different resources may be based onpolicies applied to the benefit of all current links. One strategy forPMP operation of IBRs is to use the maximum possible RF chain andantenna element resources at all times at the AE-IBR and then optimizeselectable resources at the RE-IBRs to best achieve RRC policy goals.

Note that in some deployment situations, spectrum regulations, such asthose set by the Federal Communications Commission (FCC) in the USA, mayrequire active detection of and avoidance of interference with otherusers of the spectrum (such as, for example, radar systems). The processof detecting such other co-channel spectrum users and then changing RFcarrier frequencies to another channel void of such other uses iscommonly called Dynamic Frequency Selection (DFS). Spectrum regulationsmay require that a DFS capability operate in a certain manner inresponse to certain interference “signatures” that may be detected atthe receiver of a certified radio for such spectrum. For example, someregulations require that upon detection of certain pulse lengths andreceived powers that certified radios change immediately to anotherchannel known from some minimum observation time not to have suchinterferers in operation. In some exemplary IBR implementations, suchobservations of alternative channels in advance of needing to make achange can be performed by time division multiplexing certain RF chainand antenna resources to make such measurements using RSSI and/orchannel equalization metrics reported to the RRC 660. In someembodiments, the AE-IBR and the one of more associated RE-IBRscoordinate such observations using RRC control frames to minimallydisrupt backhaul operations and maximally increase the aggregateobservation time and improve the observation accuracy. In otherexemplary IBR embodiments, at least one IBR, typically the AE-IBR, hasat least one Rx-n chain, one antenna and possibly one demodulator corepath through the IBR Channel MUX dedicated to such spectralobservations.

In embodiments with the optional IBMS Agent 700, the above channelobservation techniques of the RRC 660 can also be used in a “probe inspace” mode of operation, either at one IBR or coordinated amongstmultiple IBRs, to observe and record RF channel activity withindesignated portions of the addressable bands of operation. Such spectralanalysis information may be passed from the RRC 660 to the IBMS Agent700 for further analysis and possibly communication to other IBMS Agentsor to other databases or expert systems elsewhere within the IBRoperator's private network or to an external network such as theInternet.

Note also that the DFS operation described above is desirable forexemplary IBRs operating in spectrum bands that do not require DFSexplicitly. For example, if IBRs are deployed in licensed spectrum whereconventional PTP links operate, such conventional links generally lackthe RF carrier frequency agility and radio resource control intelligenceof the IBR. Even if the interference immunity capabilities of the IBRthrough the advantageous combinations of elements described herein issufficient to reject the interference caused by such conventional PTPlinks at the IBR receiver, it is still desirable to have the RRC 660perform DFS to avoid the converse scenario where the IBRs areinterfering with the conventional PTP links. This may be advantageousbecause it minimizes licensed band user conflicts especially if adifferent operator uses the conventional PTP equipment from thatoperating the IBRs. The presence of the conventional PTP link may bedetected in normal operation of the one or more IBRs using a particularRF carrier frequency channel or may be communicated to the RRC 660 viathe optional IBMS Agent 700 that has gathered the information fromanother source. An exemplary technique that the RRC 660 can use in anIBR where N>L and the instant SINR is approximately the same as the SNR(i.e. no significant co-channel interference) per metrics available tothe RRC 660 from the Channel Equalizer Coefficients Generator 2332 is toassign up to N minus L combinations of an antenna element 652, an Rx-nchain, and a channel MUX receive path to a Complex DFT-n to differentfrequency channels than the instant link channel to perform DFS or“probe in space” measurements and spectral analysis. For FDDconfigurations, assigning these combinations to monitor the instant orcandidate transmit frequency channels (possibly during a time when thetransmitter is otherwise inhibited) can allow the RRC to evaluatepotential interference to other conventional PTP links and to adjusttransmit resources accordingly. To the extent that the remaining atleast L receive chains provide sufficient SNR or SINR to maintain theinstant traffic load, this approach allows the RRC 660 to utilizeavailable IBR resources simultaneously for both supporting link trafficand supporting DFS or “probe in space” measurements and spectralanalysis.

As described previously, exemplary IBRs advantageously exploit thepropagation path diversity usually present in an obstructed LOSenvironment to send multiple modulated streams concurrently and thusincrease overall link throughput. For practical reasons regarding actualfield deployments, it is likely that some IBRs will be deployed inlocations where propagation may be dominated at least at some times byunobstructed LOS conditions. In such situations, IBR embodiments usingthe IBR Channel MUX 628 of FIG. 23 may not be able to resolve multiplestreams during the training Block 0 of FIG. 26 because all streamsarrive at all antennas by substantially similar paths which makescancellation for multiple demodulation streams impractical. Onealternative for the RRC 660 in this situation is to allocate one streamper link only. However, this results in reduced throughput for the linkwhich is not only undesirable but highly counterintuitive for manybackhaul operations personnel likely to perceive that unobstructed LOSshould be “better” than obstructed LOS. Thus, the RRC 660 may alsoevaluate certain antenna selection options to intentionally create pathdiversity in otherwise unobstructed or nearly unobstructed LOSconditions.

A first alternative for the RRC 660 to provide multiple streams withboth obstructed and non-obstructed LOS operation is the dynamic testingand possibly selection of mapping different modulator streams todifferent antenna elements (via separate RF chains) based on differentantenna polarizations. Because of the typically substantial signalimpairment associated with a link that is transmitting receiving fromopposite polarization antenna elements, testing of alternativepolarization antenna elements with training data may be pre-arranged intime by RRC control frames exchanged by both IBRs with an instant link.Similarly, the AE-IBR may select any changes in link antenna elementsinvolving polarization and verify an agreed upon changeover time by RRCcontrol frame exchange for reasons analogous to those for RF carrierfrequency or channel bandwidth changes. A significant advantage of usingpolarization diversity amongst the set of selectable antenna elements isthat multiple stream throughput can be maintained using a common set ofchannel equalization techniques as described above for MIMO operationwith the exemplary IBR Channel MUX of FIG. 23.

A second alternative for the RRC 660 to provide multiple streams withboth obstructed and non-obstructed LSO operation is the dynamic testingand possibly selection of mapping different modulator streams todifferent antenna elements (via separate RF chains) based on differentdirection orientations of antenna elements as is possible with exemplaryantenna arrays such as those depicted in FIGS. 14 and 15. The RRC 660 insuch IBR embodiments can test and/or change-over such multi-directionalantenna element combinations entirely at one end of a link without thenecessity of exchanging RRC control frames or requiring a coordinatedchange-over at both IBRs in a link simultaneously. For at least thepreceding reason, this second alternative to maintaining multi-streamoperation by using multi-directional antenna element combinations thatintentionally create propagation path diversity may be desirable for anRE-IBR used in a PMP configuration. An example antenna array suitablefor such an RE-IBR is depicted in FIG. 14. Furthermore, this directionalorientation diversity strategy to multi-stream operation in otherwiseunobstructed LOS is also advantageous compared to the polarizationdiversity option in PMP deployments because it does not require that theAE-IBR deploy certain resources (e.g., dedicated RF chains and antennaelements) to link modalities of benefit to some RE-IBRs but not others(that do experience obstructed LOS) as may occur with polarizationdiversity in a PMP deployment.

With reference to FIGS. 7, 32 and 33, the Intelligent BackhaulManagement System (IBMS) Agent 700 is an optional element of the IBRthat optimizes performance of the instant links at the IBR as well aspotentially other IBR links in the nearby geographic proximity includingpotential future links for IBRs yet to be deployed. As described abovein reference to the RRC 660 and depicted in FIG. 32, the primaryinteraction of the IBMS Agent 700 with the internal elements of the IBRis via a direct bi-directional path to the RRC 660. In one direction,the various policies and configuration parameters used by the RRC 660 toallocate resources within and amongst IBRs with active links to eachother are sent from the IBMS Agent 700 to the RRC 660. In the returndirection, the RRC 660 reports operational statistics and parametersback to the IBMS Agent 700 both from normal operation modes and from“probe in space” modes as directed by the IBMS Agent 700.

In contrast with the RRC 660, which communicates with other elements ofthe IBR internally or with other RRC entities at IBRs actively linked toits IBR, the IBMS Agent 700 can receive information from or transmitinformation to or initiate sessions with other elements of the overallIBMS that are logically located anywhere within any network (subject toappropriate access privileges). As shown in FIG. 32, the IBMS Agent 700appears to the overall network as an Applications layer entity thatexchanges messages typically over TCP/IP and any of the link layerinterfaces within the IBR. For the common deployment of IBRs within acellular system Radio Access Network (RAN) to backhaul cellular basestation sites, it may be necessary for the IBR to tunnel TCP/IP across acellular RAN specific transport and network layers protocol, such asGPRS Tunneling Protocol (GTP) to reach a gateway that bridges to TCP/IPand on to the desired other IBMS elements.

In some embodiments, the IBMS Agent 700 can act as an autonomous entitythat per configuration settings draws information from network resources(whether private or public) and serves as an expert system local to be aspecific IBR to optimize its performance. In other embodiments, the IBMSAgent 700 interacts with other peer IBMS Agents at other IBRs within its“interference” zone of influence via self-discovery within the immediatenetwork so that such peer IBMS Agents can collectively optimize IBRperformance within the zone. In some embodiments, the IBMS Agent 700 isa client of one or more IBMS servers that may be within the privateand/or public networks such that communications with a particular IBMSAgent 700 is always to or from or via such IBMS servers.

The information gathered at the IBR and distilled by the IBMS Agent 700regarding, for example, operational statistics (such as RSSI, channelequalization metrics, FCS failures, etc.) and resource selections (suchas antennas, channel bandwidth, modulator stream assignments, etc.), maybe sent to an IBMS server. Such information can be used by the IBMSserver to improve performance predictability of future IBR deploymentsor to enable overall IBR system performance of all links within thepurview of the IBMS server by policy optimization across IBRs. Thecommunications from the IBMS server to the IBMS Agents can include suchoptimized policy parameters based on information from other IBMS Agentsand private and/or public databases such as directories of known non-IBRlinks including their locations, antenna patterns, power levels, carrierfrequencies and channel bandwidths, tower heights, etc.

With reference to FIGS. 31 and 32, other exemplary applications layerprotocols are shown for the IBR. A Hyper Test Transfer Protocol (HTTP)server application can enable any browser (or browser-like application)on a networked computer, including a WiFi connected mobile device suchas laptop, table or smart-phone, to query or modify various IBRconfiguration parameters. The Simple Network Management System client ofFIGS. 31 and 32 is an example of an industry-standard network managementutility that can also be used to query or modify IBR configurationparameters using tools such as HP Open View.

The foregoing description of the various elements of the IBR inreference to FIGS. 5-36 have described numerous exemplary embodiments.These exemplary element embodiments may be assembled together in manydifferent combinations and permutations. A very short description of buta few of the possible overall IBR exemplary embodiments is summarizedbriefly below.

A first exemplary embodiment of an IBR includes the features outlined inTable 1.

TABLE 1 First Exemplary Intelligent Backhaul Radio Features TDDoperation PTP configuration only (AE-IBR or RE-IBR) SC-FDE modulationJmod = Jdem = 1 K = 2, M = 4 L = 2, N = 4 Q = 8, antenna array similarto FIG. 14 front facet with 2 Vertical and 2 Horizontal polarizationantenna elements at 15 dBi side facets each with 1 Vertical and 1Horizontal polarization antenna elements at 12 dBi QPSK, 16 QAM, 64 QAM,256 QAM ⅓, ½, ⅔, ¾, ⅚, ⅞ coding rates 1 or 2 modulated streams MMSEcombining of up to 4 receive chains MRC weighting of up to 4 transmitchains based on blended weights per chain across entire channel asderived from Rx conditions fixed superframe (1 ms) NACK protocol up to28 MHz channel bandwidth single MPDU per PPDU

This first exemplary embodiment can have a very high MAC efficiency(ratio of MPDU payload bits to overall MAC bits) under heavy loadingfrom the IBR LLC—in excess of 95%. Furthermore, the PHY efficiency(ratio of time where PPDU payload symbols excluding PAD are actuallytransmitted to superframe time) can exceed 90% for typical channelimpairment conditions and ranges of 2 km or less. At 28 MHz symbol rateand channel bandwidth, 256 QAM, 2 modulated streams, ⅞ rate coding, andwith MAC and PHY efficiencies of 95% and 90% respectively, the aggregatebi-directional throughput for this first exemplary IBR embodiment canexceed 330 Mb/s with an average end to end latency of about 2 ms.

A second exemplary embodiment of an IBR includes the features outlinedin Table 2.

TABLE 2 Second Exemplary Intelligent Backhaul Radio Features TDDoperation PMP configuration as the AE-IBR OFDM modulation Jmod = 2, Jdem= 3 K = 4, M = 4 L = 5, N = 5 Q = 9, antenna array similar to a 180°azimuth coverage “half-array” of FIG. 15 per each of 4 facets: 1Vertical and 1 Horizontal polarization antenna elements at 15 dBi on“top”: 1 non-polarized, 180° azimuth (aligned with array) coverage 8 dBielement connected only to the 5^(th) Rx chain and 3^(rd) demodulatorcore QPSK, 16 QAM, 64 QAM, 256 QAM ⅓, ½, ⅔, ¾, ⅚, ⅞ coding rates up to 2modulated streams per modulator core MMSE combining of up to 5 receivechains Eigenbeamforming transmit SDMA of up to 4 transmit chains fixedsuperframe (0.5 ms or 1 ms) NACK protocol TDMA alternate superframe perRE-IBR up to 2 RE-IBRs per modulator core up to 28 MHz channel bandwidthsingle MPDU per PPDU

This second exemplary embodiment uses OFDM rather than SC-FDE in orderto enable transmit SDMA of up to 4 RE-IBRs (only 2 simultaneously) in ahighly frequency selective channel. As discussed above, SC-FDE couldalso be used in this PMP AE-IBR with theoretically similar performancebut with more complex baseband processing required. This secondexemplary embodiment should have similar MAC efficiency to the first forthe 1 ms superframe case but the PHY efficiency (which needs adefinition that accounts for data block pilot subchannels andzero-padded subchannels) is typically lower with 85% being excellent.The eigenbeamforming may also require additional overheads in manypropagation environments. If 4 RE-IBRs are used in TDMA mode, thelatency would expand to 4-5 ms on average for 1 ms superframes and abouthalf that for 0.5 ms superframes. With 2 RE-IBRs that are spatiallyseparable and with operating parameters set as described for the firstexemplary embodiment above, aggregate bi-directional throughput for thissecond exemplary embodiment can be as high as about 600 Mb/s. Note thatthe “top” antenna which is not connected to a transmit chain can be usedto provide the MMSE combiner with an additional degree of freedom tocancel interference when 4 modulated streams from 2 RE-IBRs are beingsimultaneously received. It can also be used advantageously as a “probein space” to provide information to the IBMS or to assist in DFS byscanning channels not currently used at the AE-IBR. Also note thatalthough this second exemplary embodiment can be used as an RE-IBR foritself that preferably this role may be filled by the third exemplaryembodiment described below.

A third exemplary embodiment of an IBR includes the features outlined inTable 3.

TABLE 3 Third Exemplary Intelligent Backhaul Radio Features TDDoperation PTP configuration only (AE-IBR or RE-IBR) or PMP configurationas the RE-IBR OFDM modulation Jmod = Jdem = 1 K = 2, M = 4 L = 2, N = 4Q = 8, antenna array similar to FIG. 14 front facet with 2 Vertical and2 Horizontal polarization antenna elements at 15 dBi side facets eachwith 1 Vertical and 1 Horizontal polarization antenna elements at 12 dBiQPSK, 16 QAM, 64 QAM, 256 QAM ⅓, ½, ⅔, ¾, ⅚, ⅞ coding rates 1 or 2modulated streams MMSE combining of up to 4 receive chains MRC weightingof up to 4 transmit chains based on blended weights per chain acrossentire channel as derived from Rx conditions fixed superframe (1 ms)NACK protocol up to 28 MHz channel bandwidth single MPDU per PPDU

Note that while this third embodiment can also be used as a PTP AE-IBRand RE-IBR combination, it is unlikely to provide meaningful performanceimprovements for PTP compared to the first exemplary embodiment andquite possibly would have slightly lower aggregate bi-directionalthroughput and would require a less efficient and more expensive poweramplifier and stricter phase noise considerations. Forcommercially-available components today, using OFDM versus SC-FDE at RFcarrier frequencies above 10 GHz is extremely challenging. Note that forbelow 10 GHz operation, it is commercially feasible today to use SDRbaseband approaches and common chain and Front-end components to buildan IBR software programmable as either the PTP first exemplaryembodiment or the PMP RE-IBR third exemplary embodiment.

A fourth exemplary embodiment of an IBR includes the features outlinedin Table 4.

TABLE 4 Fourth Exemplary Intelligent Backhaul Radio Features FDDoperation PMP configuration as the AE-IBR OFDM modulation Jmod = 4, Jdem= 6 K = 8, M = 8 L = 10, N = 10 Q = 18, antenna array similar to FIG. 15per each of 8 facets: 1 Vertical and 1 Horizontal polarization antennaelements at 15 dBi on “top”: 2 non-polarized, opposite facing, 180°azimuth coverage 8 dBi elements connected only to the respective ones ofthe 9^(th) and 10^(th) Rx chains and the 5^(th) and 6^(th) demodulatorcores QPSK, 16 QAM, 64 QAM, 256 QAM ⅓, ½, ⅔, ¾, ⅚, ⅞ coding rates up to2 modulated streams per modulator core MMSE combining of up to 10receive chains Closed-loop eigenbeamforming transmit SDMA of up to 8transmit chains fixed superframe (.5 ms or 1 ms) NACK protocol TDMAround-robin superframe order per RE-IBR up to 4 RE-IBRs per modulatorcore up to 28 MHz channel bandwidth single MPDU per PPDU

This fourth exemplary embodiment is similar to the second exemplaryembodiment except that it utilizes a larger 360° azimuth antenna arrayand FDD operation as well as 4 time slot per modulator TDMA to supportup to 16 RE-IBRs with an aggregate bi-directional throughput of about 2Gb/s after the increased overhead in efficiencies of the system areaccounted for. Latency also increases proportionately if 4 TDMA slotsare used.

A fifth exemplary embodiment of an IBR includes the features outlined inTable 5.

TABLE 5 Fifth Exemplary Intelligent Backhaul Radio Features FDDoperation PMP configuration as the RE-IBR OFDM modulation Jmod = Jdem =1 K = 2, M = 4 L = 2, N = 4 Q = 8, antenna array similar to FIG. 14front facet with 2 Vertical and 2 Horizontal polarization antennaelements at 15 dBi side facets each with 1 Vertical and 1 Horizontalpolarization antenna elements at 12 dBi QPSK, 16 QAM, 64 QAM, 256 QAM ⅓,½, ⅔, ¾, ⅚, ⅞ coding rates 1 or 2 modulated streams MMSE combining of upto 4 receive chains Selected unweighted Tx antennas as directed byreceiver at opposite end fixed superframe (1 ms) NACK protocol up to 28MHz channel bandwidth single MPDU per PPDUThe primary application of this fifth exemplary embodiment is to serveas an RE-IBR for the fourth exemplary embodiment AE-IBR.

A sixth exemplary embodiment of an IBR includes the features outlined inTable 6.

TABLE 6 Sixth Exemplary Intelligent Backhaul Radio Features FDDoperation PTP configuration only (AE-IBR or RE-IBR) SC-FDE modulationJmod = Jdem = 1 K = M = 2 L = 2, N = 4 Q = 6, antenna array similar toFIG. 13 3 Vertical polarization antenna elements, 2 at 13 dBi and 1 at18 dBi, 3 Horizontal polarization antenna elements, 2 at 13 dBi, 1 at 18dBi QPSK, 16 QAM, 67 QAM, 256 QAM, 1024 QAM ⅓, ½, ⅔, ¾, ⅚, ⅞, 9/10coding rates 1 or 2 modulated streams MMSE combining of up to 4 receivechains selection of 2 antennas in transmit fixed superframe (1 ms) NACKprotocol up to 56 MHz channel bandwidth single MPDU per PPDU

This sixth exemplary embodiment provides high aggregate bi-directionalthroughput of up to about 1.8 Gb/s with moderate complexity relative toother IBRs. This sixth exemplary embodiment performs optimally inpropagation channels with only moderate obstructions compared tounobstructed LOS. FDD also provides <1 ms average latency.

A seventh exemplary embodiment of an IBR includes the features outlinedin Table 7.

TABLE 7 Seventh Exemplary Intelligent Backhaul Radio Features FDD/TDDhybrid operation PTP configuration only (AE-IBR or RE-IBR) SC-FDEmodulation Jmod = Jdem = 1 K = 4, M = 8 L = 4, N = 8 Q = 12, antennaarray similar to FIG. 14 per each of 3 facets: 2 Vertical and 2Horizontal antenna elements of 15 dBi each QPSK, 16 QAM, 64 QAM, 256 QAM⅓, ½, ⅔, ¾, ⅚, ⅞ coding rates up to 4 modulated streams MMSE combiningof up to 8 receive chains MRC weighting of up to 8 transmit chains basedon blended weights per chain across entire channel as derived from Rxconditions fixed superframe (1 ms) NACK protocol up to 56 MHz channelbandwidth single MPDU per PPDU

This seventh exemplary embodiment has additional resources compared tothe sixth exemplary embodiment to provide higher aggregatebi-directional throughput of about 3 Gb/s for a PTP link with <1 mslatency that can operate in a severely obstructed LOS propagationchannel. It advantageously uses hybrid FDD/TDD operation wherein eachfrequency duplexed channel alternates in opposite synchronization toeach other between transmit and receive. This enables a relativelystraightforward and efficient transmit chain weighting to be derivedfrom receive chain equalization analysis without increasing latency.Furthermore, an additional degree of frequency diversity (and space tothe extent different antennas are selected) is achieved. The FDD/TDDhybrid can be utilized on any FDD IBR deployment where spectrumregulations permit it. To the extent each FDD band operation relies onband-specific band-select filters in the Front-ends, then additionalcircuit complexity for switching between transmit and receive is needed.

Note that the preceding embodiments are a small subset of the possibleIBR embodiments that are enabled by the disclosure herein. Note furtherthat many additional optional structures or methods described herein canbe substituted within the above exemplary embodiments or otherembodiments.

For example, TDD CSMA could be used advantageously in high interferencespectrum allocations or where required by spectrum regulations as asubstitute for fixed superframe timing in the above exemplaryembodiments.

Note also that all of the above exemplary embodiments are compatiblewith any RF carrier frequencies in the range of interest fromapproximately 500 MHz to 100 GHz.

Note further that in multi-channel embodiments, it is possible to usedifferent access and MAC protocols in different channels especiallywhere advantageous for or required by spectrum regulations. For example,an IBR link may advantageously provide a “base” throughput capability ina channel expected to have minimal interference but for which licensingcosts or regulatory restrictions limit total throughput. Then a “surge”throughput capability can be provided in a second channel, such asunlicensed spectrum, where throughput can be higher but the risk oftemporal interference outages is also higher.

As evident from the above exemplary embodiments, OFDM is typically usedfor PMP deployments because at a baseband processing level it isrelatively less complex than SC-FDE if frequency-selective channels areto be used with transmit SDMA (at least at the AE-IBR). However, OFDMhas higher peak to average ratio and is more sensitive to carrierfrequency offset and phase noise than SC-FDE. Thus, for PTP, SC-FDE isoften preferable, especially for operation at RF carrier frequenciesabove 10 GHz where commercially viable components are expensive foreither OFDM power amplification or OFDM-compatible local oscillatorspecifications.

Note that in backhaul applications where links are nominally continuous,additional techniques can improve PHY efficiency. For example, withOFDM, the training block can be combined with a PLCP Header block byinterleaving subchannels appropriately. This is also possible for SC-FDEif DFT pre-coding (i.e. Tx block Assembler-k includes a DFT and Tx-Mux-mincludes an IDFT) is used. DFT pre-coding for SC-FDE can also be used topulse shape the transmitted waveform similar to OFDM zero padding and/orwindowing. The training block in SC-FDE can also be shorter than thedata blocks to save PHY overhead by either using another FFT fortraining or switching the FFT bin size during the training block. Thechannel equalization function so derived is then interpolated for use onthe longer data blocks with additional frequency bins. Also, when usingDFT pre-coding in SC-FDE, it is possible to time multiplex an FFT blockbetween transmit and receive or within transmit or receive such that allfour FFT operations of an SC-FDE transceiver can be realized by 2 oreven 1 FFT hardware core. Another technique to simplify PMP deploymentof IBRs is to use OFDM in the forward link from AE-IBR to the multitudeof RE-IBRs, and then use SC-FDE in the reverse link from RE-IBR toAE-IBR. This enables the advantages of transmit eigenbeamforming at theAE-IBR in a frequency-selective channel based primarily on receiveequalization while keeping the RE-IBRs relatively straightforward withmuch simpler transmitters than in the OFDM only case.

Numerous additional variations of the above-described elements of theIBR can also be advantageously utilized in substitution for or incombination with the exemplary embodiments described above. For example,antenna elements need not always be shared between transmit and receivewhether in TDD or FDD mode. In certain embodiments, it is preferable tohave a smaller number of transmit antenna elements, often with broaderazimuthal coverage than those used by the receive antenna elements, thatare always used versus a selectable larger number of receive antennaelements. In some embodiments with separate transmit and receive antennaelements, the respective front-ends of FIGS. 11 and 12 would not requirerespectively the SPDT switch or the band selection within a duplexerfilter and either the receive path elements for a front-end coupled to atransmit antenna element or the transmit path elements for a front-endcoupled to a receive antenna element, which further advantageouslyreduces cost and complexity of the IBR. In such embodiments, eachtransmit antenna element is coupled to a respective transmit poweramplifier which is in turn coupled to a respective transmit RF chainwherein such couplings may be selectable RF connections or fixed RFconnections—the latter for IBR embodiments wherein certain transmit RFchains are always connected to certain transmit power amplifiers andcertain transmit antenna elements whenever the IBR is in a transmitmode. Similarly, each receive antenna element is coupled to a respectivereceive low noise amplifier which is in turn coupled to a respectivereceive RF chain wherein such couplings are typically selectable RFconnections as described herein.

As another example, the NACK protocol described above with reference toFIG. 33 and various IBR embodiments can be extended to either ACK/NACK,single NACK as described above, or persistent NACK until delivered.Furthermore, such exemplary choices can be applied to individual MSDUsbased on either an indicator from the IBR LLC of FIG. 33 or inspectionof MSDU class of service or type of service header field bits as definedby a policy either within the IBR MAC or updateable via the optionalIBMS Agent 700. For example, MSDUs corresponding to Voice over InternetProtocol (VoIP) packets are typically sent at a high class of servicepriority but with so little tolerance for latency that it may bepreferable to send such MSDUs with no ACK/NACK retransmission option orwith only the single NACK protocol described previously. At the oppositeextreme, certain data transfers, such as for example only, cellularnetwork control or management plane messages or user file transfer data,may tolerate considerable or unpredictable latencies associated withpersistent retransmission until NACK=0 rather than rely on much slowerupper layer retransmission protocols. The policy for mapping MSDUs to aparticular ACK/NACK strategy may also be responsive to radio channelconditions and/or loading as determined within the various elements ofthe IBR described above. For example, when the current packet failurerate is very low and/or the loading demand on the IBR is high comparedto the capacity of the MCS, then one policy may be to minimizeretransmissions by transmitting most MSDUs with no ACK/NACK or a singleNACK. Alternatively, for a high packet failure situation and/or lowdemand at a given MCS, the opposite strategy may be used. Also, any ofthe IBR embodiments described herein that use copper Ethernet interfacesmay also use such interfaces to supply Power over Ethernet (PoE) to theIBR.

FIGS. 37-45 illustrate a Hybrid Band Intelligent Backhaul Radio (HB-IBR)according to certain embodiments of the invention. The HB-IBR includestwo radios, each operating in a different band. In some embodiments, theHB-IBR includes two IBRs, as described above with reference to FIGS.5-36. In other embodiments, the HB-IBR includes an IBR in combinationwith another radio, such as a CBR (conventional backhaul radio), asdescribed above with reference to FIGS. 1-4. In some embodiments, theHB-IBR includes a dual radio configuration in which the first radiooperates in a non-line of sight (NLOS) radio link configuration and thesecond radio operates in a near line of sight (nLOS) or line of sight(LOS) radio link configuration. In some embodiments, the differentoperating bands are a high band and a low band.

FIG. 37 illustrates an HB-IBR 3700 in accordance with one embodiment ofthe invention. In the embodiment shown in FIG. 37, the HB-IBR includesan IBR operating in the non-line of sight mode of operation within the5.8 GHz ISM band 3701 _(E), and a CBR as an ancillary radio linkoperating in the FCC part 101 E band of operation at 71 to 76 GHz 3701_(ISM). It will be appreciated that the radios may one or both of theradios may operate in different frequencies band. For example, the nLOSor LOS radio (3701 _(E)) link may operate within the 57 GHz CFR 47 Part15.247 ISM unlicensed band, an alternative Part 101 bands of operation,or yet other bands.

In FIG. 37, a common medium access control (MAC) block 3702 is utilizedbetween the dual radios 3701 _(E) and 3701 _(ISM). The common MAC 3702allows for specific advantages in installation and operation. It will beappreciated that in alternative embodiments, each radio may have aseparate MAC bock, and the MAC blocks of each of the radios maycommunicate with one another.

In some embodiments, blocks 616 _(E) through 660 _(E) the nLOS/LOS radio(3701 _(E)) may be the same or similar to the respective blocks 616through 660 described above with reference to FIG. 6. Likewise, in someembodiments, blocks 616 _(ISM) through 660 _(ISM) of the NLOS/LOS radio(3701 _(ISM)) may be the same or similar to the blocks 616 through 660described above with reference to FIG. 6.

It should be noted that there is no relative relationship inferredbetween the relative dimensions of instantiations of IBR blocks 3701_(E) and 3701 _(ISM) with respect to the number of antennas (Q_(E),Q_(ISM)), RF receivers (M_(E), M_(ISM)), RF transmitters (N_(E),N_(ISM)), or receiver or transmitted streams (K_(E), K_(ISM), L_(E),L_(ISM)).

In the embodiment of FIG. 37 (and other embodiments of the HB-IBR)signaling between the a low band or NLOS radio link (utilizing the ISMband link 3701 _(ISM) in an example embodiment) and an upper band or LOSradio link (utilizing an E band link 3701 _(E) an embodiment) may becoordinated. For example, the NLOS (5.8 GHz in some embodiments) linkmay be used for the transport of control frames, acknowledgment frames(or negative acknowledgement frames) or the like, while the nLOS (nearline of sight) or LOS (line of sight) link in the E Band may be usedprimarily or entirely to transport data payload. The control frames mayinclude antenna control messaging or metrics feedback for the purpose ofantenna control at the transmitting radio to allow for the adjusted andoptimized (self-healing) operation of the radios. Other controlsignaling may include use of signaling between the MAC, RLC, or RRCentities. In some embodiments, the modulation and coding scheme (MCS)may be signaled, while, in other embodiments, coordination ofoperational frequencies may be performed, while, in yet otherembodiments, coordination of retransmissions of data received in errormay be signaled. For example, the coordinated signaling may be used whenadaptive transmitter beam forming is utilized within an IBR point topoint E-band link, which is coordinated and managed utilizing the NLOSlink. In another example, the NLOS link may be used to aid in thealignment of the nLOS link by providing metrics or commands for use inthe control of a servo motor (or otherwise motorized alignmentmechanism) to adjust the antenna. Such servo motors may be used toperform adjustments to the azimuth or elevation of a fixed dish typeantenna for the nLOS link, the NLOS link being able to be used toperform an initial or continual optimization of the nLOS or LOS link.

In FIG. 37, the radios share a common MAC (3702), but each radio has adistinctly separate RRC (656E, 656ISM), RLC (660E,660ISM), MODEM (624E,624ISM), and associated radio blocks. In other embodiments, the radiosmay be entirely separate (i.e., no common MAC 3702), but with acoordinating function between the MAC entities for each radio at eachrespective HB-IBR site.

The HB-IBR provides significant advantages relative to current E BandCBRs. For example, the HB-IBR requires a reduced installation time forthe equipment and point to point link configuration. The cost ofinstallation is additionally reduced because the required proficiency ofthe individuals performing the installation is lower. In addition, thenumber of individuals required to perform the installation may bereduced. In addition, the precision of the alignment of the nLOS fixedantennas may be greatly simplified and may, in some cases, be performedremotely. Such embodiments may additionally provide for a more optimalinitial installation and ‘survey” of various reception parameters, whichcan be used in the determination of an optimization metric at each ofthe motorized nLOS or LOS radios to determine the most robust, highestperformance or most otherwise optimum alignment of the nLOS or LOS linkantennas.

In some embodiments, a more optimal initial installation may beperformed, in which a ‘survey” of various reception parameters may beused as an optimization metric, at each of the motorized nLOS or LOSradios to determine the most robust, highest performance or mostotherwise optimum alignment of the nLOS or LOS links antennas. In someembodiments, performance of the HB-IBR may be improved because initialoperating parameters (e.g., antenna positions) may be selected so thatthe link performances are less susceptible to variations in theinstallation or operating environment (e.g., structure vibration,temperature changes, rain fades, etc.).

In some embodiments, the control and coordination between the NLOS andnLOS/LOS links allow for a self-healing capability (allowing for thenLOS/LOS link to be continually optimized). Such optimization may beuseful in conditions where a nLOS link is modified by the growth oftrees, or their structural changes to the propagation environment.

Additional benefits of embodiments of the HB-IBR include a reducedlatency of the payload on the LOS link when the LOS link is operated inTDD mode, and when the NLOS link is utilized for the signaling for theneed for re-transmissions (ACK/NACK), allowing for a faster response todropped radio FEC blocks. This is the result of not requiring the delayin sending the ACK/NAK signaling of the time division duplexed (TDD)return path on the LOS link.

In some embodiments, the HB-IBR allows for a redundant data linkcapability for high priority traffic. For example, in the case of a LOSor nLOS link outage, specific classifications of QOS packets or otherpackets may be sent over the lower data rate NLOS link, while otherclassifications of packets may be either queued or discarded. Suchembodiments ensure the most critical traffic continues to be delivered,while less critical traffic may be delayed or undelivered. Such trafficclassification may be based on, for example, MPLS, 802.1p, DSRC,IntServ, DifServ, or other related QOS, priority, or otherclassification schemes as known in the art.

With reference back to FIG. 37, specific signaling associated with theuse and configuration of the E band radio link (or upper band link)operated by Radio 3701E allows for payload data to be between arespective E band radio at a respective HB-IBR, whereas controlsignaling, redundant data, or re-transmissions of data may becommunicated by a non-line-of-sight (NLOS) radio link operated by Radio3701ISM. The MAC entity (3702) communicates with E band Radio 3701Eutilizing TX data line 601E and RX data line 620E and furthercommunicates with the ISM band radio utilizing TX data line 616ISM andRX data line 620ISM. Control lines from the MAC entity also communicatewith the radio resource control blocks (RRC) and radio link control(RLC) blocks of the respective E band and ISM band radios.

As explained in further detail hereinafter, acknowledgements (ACK) ornegative acknowledgements (NAK) associated with a re-transmission schememay be sent. Such re-transmission schemes apply to data sent on the Eband radio, and re-transmission control signals may be sent on the ISMband radio link. Alternatively, or in addition, the actualre-transmissions of data received in error on the E band nLOS link maybe sent on the ISM band NLOS link.

In some embodiments, the ISM band radio link may carry control messagingassociated with the modulation and coding selection (MCS) which iscurrently in use on the E band radio. Furthermore, in some embodiments,the E band receiving HB-IBR may send signals requesting specific MCSmodes of operation from the E Band transmitting link utilizing the ISMradio link. Such modulation and control signaling may be based upon thereceiving station evaluating the Eb/Io, EVM, SNR, and the like todetermine a desired modulation and coding based upon the evaluation ofreceived parameters and communicated back to the transmitting HB-IBR ofthe E band nLOS link.

In embodiments utilizing ISM band control and management, communicationsrelating to the MCS coding may also be performed by transmittingmessaging utilizing the ISM band link, indicating modulation and codingwhich is currently, or will be in effect for the data being received onthe respective E band HB-IBR receiver.

It will be appreciated that in the above described embodiments, thecommunications may be performed on a per spatial stream basis, or on aper frequency band, carrier, or sub-carrier basis. In other embodiments,control of all streams, channels, carrier and sub-carriers may beperformed simultaneously.

Additionally, the forgoing signaling approaches may be used to controlthe transmission power from an upper band or E band transmitting HB-IBR.Such control may be for all transmission, or on a per stream, carrier,or sub-carrier basis. Such techniques have the advantage that only therequired transmit power is utilized as determined by the receiving Eband radio, and signaled in return over the ISM band link, thus closingthe control loop.

In some embodiments, the HB-IBR may perform transmit beam formeroptimization when multiple antennas are utilized for transmission withinthe E band link associated with Block 3701E also of FIG. 37. In someembodiments, the control feedback from a receiving E band HB-IBR stationmay also be performed utilizing the ISM band link. In some embodiments,such feedback may be used in determining additional transmissionparameters such as transmit antenna selections or transmit beam formerweights and the like.

In some embodiments, parameter determination may be performed at thereceiving E band HB-IBR and communicated back to the transmitting HB-IBRutilizing ISM link. Alternatively, so-called channel state information(CSI) as known in the industry, or other receiver metrics may be sentback from the receiving E band HB-IBR over the ISM band to thetransmitting E band HB-IBR. As a result, various E band transmit antennaparameters and other radio link configuration parameters may beoptimized based on such E band receive HB-IBR station parameters. Suchreceive parameters may include channel state information, signal tonoise ratio, receive channel delay spread, interference levels, receivesignal levels, and the like.

In some embodiments, interference levels are measured at the receiving Eband HB-IBR. Such feedback information may also include informationrelative to the determination of jamming signals from unwantedinterferers operating in one or both bands and communication links. Suchinformation may further be used for the determination of transmitternull steering such that interference to other stations is minimized orreception null steering such that interference from other stations isminimized. Such techniques allow for a more optimal performance of the Eband communications link between respective HB-IBRs.

In some embodiments, a fixed dish antenna may be utilized for E bandradio 3701E. In such embodiments, a single large aperture fixed dishantenna may be used or a plurality of smaller, directive antennas may beutilized. However, as the E band operates in specific frequencies withinthe 71 to 95 GHz range, the gain required for desirable range providedby such directive antennas generally requires a relatively narrow beamwidth as discussed previously in this disclosure. As a result, someembodiments may utilize motorized positioning of the fixed dish antennaor multiple antennas for use with the E band link associated with 3701E.In these embodiments, one or more fixed antennas interface with IBRantenna array block 648E and are associated with Antenna Elements 1through QE.

The foregoing control and communication arrangements may be utilized forcontinual optimization during operation of ISM and E band links betweenthe HB-IBR of FIG. 37 and a respective HB-IBR, forming pairedcommunication links.

FIG. 38 illustrates a process 3800 for installing an HB-IBR, such as theHB-IBR of FIG. 37. It will be appreciated that the process 3800 may beused for the installation of the various embodiments of the HB-IBRdescribed herein. It will also be appreciated that other processes maybe used to install the HB-IBRs described herein, and that the process3800 may vary from that shown in FIG. 38. For example, the order of someof the steps may be different and/or the process 3800 may include feweror additional steps.

The process 3800 may be used during the initial installation process,allowing for an ease of installation, a faster installation and theability for less qualified technicians to perform such installations.These advantages allow for a reduced cost and enhanced suitability tovarious deployments where performance, reliability, and cost arecritical.

As shown in FIG. 38, the process 3800 begins with the physical mountingof a first HB-IBR at a location where it is aligned to within a grossalignment tolerance (block 3801). Such gross alignment may utilize aninstallation assisting device which allows for a magnetic compassalignment of the first HB-IBR to within plus or minus 20 degrees of a“bore-sight” alignment to the prospective installation site of a secondHB-IBR. In one embodiment, the installation of a first IBR may includeserver motors which are subsequently used for a fine alignment of thetransmit and receive directive antennas for the HB-IBR E band antennasfor each HB-IBR. An initial tolerance for the coarse alignment at block3801 is based upon the range of angular adjustment in azimuth andelevation of the servo motors (or other motorized adjustment mechanisms)associated with the HB-IBR E band antennas.

Embodiments of the antennas include, for example, a combined ISM,non-line-of-sight (NLOS) antenna and a near-line-of-sight orline-of-sight (“(n)LOS”) antenna in a single physical arrangement, suchthat server motor adjustments to the E band antenna additionally movesthe ISM band antenna(s) together as a single adjustment. As a result, itis contemplated that alignment of the near-line-of-sight (nLOS) or lineof sight (LOS) antenna array would allow for an operational alignment ofthe non-line-of-sight, NLOS antennas as a consequence of the E bandantenna alignment. Such non-line-of-sight (NLOS) antennas have differentantenna patterns from those of the higher band antennas for use with the(n)LOS radios. However, the NLOS antenna pattern beam widths aregenerally wider than those of the (n)LOS antennas, allowing for moreflexibility in installation. In other embodiments, the server mechanismsmay adjust only the E band or (n)LOS link antennas, while the NLOSantennas are adjusted separately. It will be appreciate that the initialplacement at block 3801 may be performed by a technician to within theinitial coarse alignment tolerage.

The process continues by installing a second HB-IBR B within therequired course alignment tolerance as descried above (block 3801), andestablishing a non-line-of-sight (NLOS) link between the initiallyinstalled HB-IBR A and the installed HB IBR B (block 3802). Thenon-line-of-sight link between the two HB-IBRs is then used for finealignment of the line-of-sight or near-line-of-sight link. Because theISM band antennas allow for a wider range of installation alignments, ormay be installed with a separate alignment, the ISM link continues toremain in operation while E band antenna alignment adjustments asdescribed below. In some embodiments, the fine alignment of the E bandantennas is performed using said server motors. In alternativeembodiments, rather than using server motors, beam steering approachesmay be used with a multiplicity of transceivers in the place of theserver motors. However, for the purpose of illustration, the process3800 shown in FIG. 38 is described using of server motors at bothHB-IBRA and HB IBRB and with integrated antennas for each HB-IBR betweenthe respective ISM and E band radio antennas.

The process 3800 continues by improving the performance of thecommunication link between HB IBR A and B over the non-line-of-sight(NLOS) link in the ISM band (at 5.8 GHz), such that the fine alignmentprocedure is utilized (block 3803). The procedure described in blocks3803 to 3808 utilizes the NLOS link to perform a multi-dimensional scanprocess at each of the HB IBRs in various positions of the (n)LOSantennas. In some embodiments, the scan process involves positioning theE Band directional antenna of one HB-IBR at a specific azimuth andelevation (block 3804), and then performing multiple measurements at therespective HB-IBR utilizing its E band antenna at a specific azimuth andelevation (block 3805). Multiple metrics based upon the received signalmeasurements and the current antenna positions are calculated and stored(block 3807). Once the current antenna positions are characterized,additional antenna positions are selected and the process is repeated,until it is determined that the combinations of HB-IBR antennaalignments are sufficiently characterized (block 3808). It will beappreciated that a significant number of HB-IBR A and BH-IBR B positionsmay be required for a sufficient characterization in multiple dimensionsbetween the two stations for the E band (n)LOS link.

The above-described multi-dimensional scan process allows for thecollection of metrics between the two radios for reception andtransmission. In some embodiments, return transmission may be made fromHB IBR B to HB-IBR A. In some embodiments, metrics may be calculated inalternative directions of transmission or locations. In some embodimentsutilizing frequency division duplexing (FDD), measurements may berequired in multiple frequencies of operation and for varying directionsof transmission between HB-IBRA and HB-IBRB. In some embodimentsutilizing time division duplexing (TDD) operation of the E band link,measurements may need only be performed for one frequency band ofoperation, but it may still be advantageous to perform the scan in bothdirections of transmission between the HB-IBRs in cases whereinterference from other nodes is being evaluated such that it may beconsidered in the selection of a configuration for normal operation ofthe (n)LOS link.

Exemplary metrics that are collected include, for example, signal tonoise ratio, received power, signal to interference, Eb/No, Eb/Io, andthe like. Other exemplary metrics include channel response, spatialrichness, number of spatial modes of propagation, level of independenceof antenna characteristics, antenna cross pollination performance, Rx/Txantenna isolation performance and other properties known in the art, anddiscussed elsewhere within this disclosure. The collected metrics may beused for the initial selection of parameters for optimization foroperation of the E band radio link (block 3809). This selection andoperation may be controlled utilizing control messaging over the ISMband non-line-of-sight link.

FIG. 39 is a timing and message flow diagram illustrating the timing ofsignals for an embodiment of an HB-IBR with a time division duplexed(TDD) based radio protocol for both an E Band (n)LOS link and for a 5.8GHz ISM NLOS link. The Y axis of FIG. 39 shows the “Channel Activity.”The “Channel Activity,” which includes received and transmitted radioframes, for the E band radio is shown in the top half of FIG. 39. Asshown in FIG. 39, the transmitted E-Band frames are labeled E_Tx-j andthe received E Band frames from the E-Band are labeled E_Rx-j. Thechannel activity for the NLOS radio is shown in the lower half of FIG.39. As shown in FIG. 39, transmission of the jth ISM radio frame islabeled ISM_Tx-j, and reception for the jth ISM radio frame is labeledISM_Rx-j. Exemplary receive and transmit frames (3901, 3902, 3903, 3907for example) are shown as channel activity versus time in the timingdiagram. The timing relationship between the E band transmit frames(e.g., frame 3901) and receive E band frames (e.g., frame 3902) relativeto the transmit ISM band frames (e.g., frame 3903) and receive ISMframes (e.g., frame 3904) are shown in FIG. 39.

It is advantageous in embodiments of time division duplexed systems toreduce the timing latency of the media access control protocol relativeto the generation and reception of acknowledgements or negativeacknowledgements from a receiver back to the transmitting station suchthat the retransmission of packets, or frames in this case, are achievedwith as little latency in time as possible. Such latency is adisadvantage of conventional time division duplexed systems utilizing asingle radio link utilizing a TDD protocol. The latency is an inherentresult of the need to wait for the transmission period of the link whena negative acknowledgement (NACK) is transmitted in response to a blockor a frame received requesting a re-transmission. Following the inherentdelay in the retransmission request, additional delay is incurred as aresult of the actual re-transmission being required to wait for the nextTX duplex time period to send the requested retransmission of the blockor frame received in error. Such TDD latency disadvantages may beaddressed in utilizing a hybrid band radio configuration where two linksare utilized, with shared and coordinated MAC level processing as thecontrol frames such as ACK, NAK, or both may be generated immediatelyand sent over the second radio link, defeating the requirement to whatfor the subsequent transmission time period for ending such control ormanagement signaling.

In some embodiments, a specific timing offset between a transmit framein the E band and a receive frame in the ISM band, ΔT_(E) _(—) _(ISM)_(—) , is adjusted to minimized delays for retransmission requests, andother associated messaging and payload communications. Such timingoffsets allow for a reduction in the latency of the protocol foracknowledgements and negative acknowledgements for the E band. As shownin FIG. 39, frame 3902 includes a block 3906. If, for example, duringreception of frame 3902, a specific block within frame 3902 is receivedin error, feedback relative to a particular block within the frame 3902(the NACK) may be provided by the transmit signal contained within theISM transmit frame (3903). The control signaling indicating thisfeedback is shown as logical coupling 3905 a to 3905 k. The time delayto determine if a block received as part of receive E band Frame 3902 isin error or is received correctly is performed faster than the relativetiming offset ΔT_(E) _(—) _(ISM). As a result, it may be determined thatthe first block in frame 3902 is received correctly or in error, andfeedback 3905 a is provided to block 3903 prior to transmission of thatblock. Hence, the latency in such control feedback may be greatlyminimized relative to conventional TDD based systems. For the last block3906 of frame 3902, the acknowledgement may be provided as a final blockwithin ISM Transmit frame 3903. However, to retransmit the dataassociated with block 3906, E band reception time period latency must betolerated. Such a delay in retransmission of the data received in errormay defeat many of the benefits in latency reduction of the arrangement.In some embodiments, an approach to address this potential deficiency isto send the actual transmit block data (3906) if received in errorwithin the ISM band as a “clean up” process as block 3907. This approachavoids a significant amount of the time latency in re-transmissionrequired within the ISM band because it does not wait for the next timedivision duplexed receive time within the E band, thus reducing overalllatency of the link.

Utilizing the E band for payload transfer and the ISM band for thereturn of acknowledgements or negative acknowledgements or both, inaddition to the “clean up” blocks, provides a reduction in the timingrequired to perform the feedbacks. Such techniques greatly reduce theoverall latency, which is problematic in convention time divisionduplexed protocols. The relative timing offset ΔT_(E) _(—) _(ISM) may beadjusted or selected based upon the time to determine the correctreception or incorrect reception status of a particular block within anoverall received E band frame. In alternative embodiments, the ISM frameneed not be a time division duplexed protocol, but may utilize afrequency division duplexed protocol in a similar manor to achievesimilar benefits in the E band latency reduction. It will be appreciatedthat in other embodiments, the same bands need not be used. Rather, anycombination of a “lower” and an upper band may be utilized.

Referring now to FIG. 40, a depiction of a hybrid-band intelligentbackhaul radio configuration is shown wherein a conventional CellularBackhaul Radio 4002A is paired with an Intelligent Backhaul Radio 4003Ato form a Hybrid-Band Intelligent Backhaul Radio HB-IBR 4000A.Hybrid-Band Intelligent Backhaul Radio 4000A also includes a servo motor4001A, a dish type antenna 4005A, and an antenna array 4004A.

Dish Antenna 4005A communicates in the E-Band frequency range utilizinglink 4010 with a respective Hybrid-Band Intelligent Backhaul Radio 4000Butilizing Dish 4005B. In FIG. 40, the transceiver of CBR 4002A iscoupled with dish 4005A utilizing cable assembly 4007. A 5.8 GHz ISMBand Link 4020 is established between Hybrid-Band Intelligent BackhaulRadio 4000A utilizing Antenna Array 4004A and HB-IBR 4000B utilizingAntenna Array 4004B. Antenna array 4004A is coupled with IBR 4003Autilizing a cable assembly 4006.

It will be appreciated that the E-Band link 4010 and ISM Band link 4020may vary from that shown in FIG. 40. For example, rather than utilizingan E Band link as the “Upper Band,” various other bands may be utilizedas the Upper Band, including, for example, 23 GHz, 38 GHz, 57 to 64 GHz,71 to 76 GHz, etc. In another example, the “Lower Band” may utilizeother frequency bands, including, for example, 2.4 GHz, 3.5 GHz, 5.2GHz, etc., and other ISM or non-ISM designated bands.

In FIG. 40, two functionally-equivalent HB-IBRs are utilized tocommunicate over the pair of radio frequency channels 4010 and 4020. Theservo motor 4001A is operative to control the positioning of the dishantenna 4005A under the control of IBR 4003A and/or CBR 4002A. Inparticular, in FIG. 40, control line 4008 carries signaling from IBR4003A. This control signaling may include, for example, messaging,voltages, currents, encoded control signals, and the like. Although aservo motor is shown in FIG. 40, it will be appreciated that otherpositioning mechanisms may be used to control the positioning of thedish antenna 4005A, including but not limited to: linear positioners,rotary actuators, sliding actuators, linear slides, belt drivenactuators, screw drives, and the like.

A shared media access controller (e.g. MAC 3702 shown in FIG. 37), maybe utilized to control IBR 4003A and also interface with CBR 4002A. TheMAC controller 3702 may be included within IBR 4003A.

FIG. 41 illustrates an alternative embodiment of the hybrid bandintelligent backhaul radio HB-IBR. The embodiment of the HB-IBR of FIG.41 differs from the embodiment of the HB-IBR of FIG. 40 in that anantenna array is used for the upper band radio 4105 instead of a dishantenna. The functionality of IBR 4003A and CBR 4002A are largely thesame in the embodiments of FIGS. 40 and 41. It will be appreciated thatthe control 4008 of FIG. 41 is modified to provide control signalingappropriate for the control of an electronically steerable antenna array4105 for the upper band. In both the embodiments of FIGS. 40 and 41,cable assemblies 4007 and 4006 may support cross-polarization signalsfor both a vertical and a horizontal polarization configuration for bothreception and transmission.

Positioning of the antenna array in FIG. 41 may be accomplished using aservo motor (or other positioning mechanism), as described above withreference to FIG. 41. Alternatively, the high band antenna array 4015may be electronically steered by approaches known in the art including,for example, the use of a phase array configuration, or otherapproaches. In other embodiments, a combination of electromechanical andelectronic steering may be used to position the antenna array 4015.

FIG. 42 illustrates an exemplary physical configuration of the HB-IBR ofFIG. 40. Upper band dish antenna 4005A is positioned with antenna array4004A in close proximity to and physically mounted rigidly with the dish4005A. Antenna array 4004A is partitioned into sub array sections 4004A1and 4004A2 such that half of the antenna array 4004A1 is located on oneside of dish antenna 4005A and the other half of antenna array 4004A2 islocated on the other side of dish antenna 4005A. In FIG. 42, the subarray 4004A1 is below the dish antenna 4005A and the sub array 4004A2 isabove (or otherwise on the opposite side of) the dish antenna 4005A. Thetwo sub arrays 40041A1 and 4004A2 are positioned with a ten degreeoffset relative to the bore sight angle of the antenna dish for theupper band 4005A. In FIG. 42, sub-array 4004A2 is positioned with a tendegree elevation increase while sub-array 4004A1 is positioned with aten degree declination relative to bore sight for dish 4005A. It will beappreciated that this arrangement is merely exemplary, and alternativerotational orientations, and alignments of the sub-arrays and dishantennas are contemplated. In addition, the sub-arrays need not bepositioned above and below the dish, but may be in any orientation,including horizontal, vertical or otherwise.

As discussed with respect to FIG. 40, cable assembly 4006 connects thetransceiver of IBR 4003A with antenna array 4004. However, in this case,different signals may carried over the cable assembly 4006 and appliedto and partitioned for each sub-array 4004A2 and sub-array 4004A1. Inthe embodiment shown in FIG. 42, cable assembly 4006 includes eight RFlines or cables. Such cables provide for two antenna elements, each withcross-polarization capability, resulting in four RF signals beingcoupled to and from sub-array 4004A2 utilizing cable subassembly 4006B.Likewise, four RF couples are coupled to sub array 4004A1 utilizingcable subassembly 4006A. Alternatively, fewer RF signals may be used(e.g., four or even fewer signals instead of 8 signals) by utilizingswitching associated with one or more of the antenna elements forpolarization selection, selection of one or more of a subset of theelements themselves, or groups of antenna elements.

Additional control signaling may be included within the cableassemblies, as well as power and grounding and associated conductors, asknown in the art. In some embodiments, the additional control lines maybe used for the control of the previously mentioned switched, for Rx/TXswitching control, AGC, TX power control, or any other control, as knownin the art.

FIG. 43 illustrates an exemplary physical structure of the HB-IBR ofFIG. 41, including the physical relationship between the upper bandantenna array 4105 and the lower band antenna array 4004A. As describedabove with reference to FIG. 42, sub-arrays 4004A2 and 4004A1 areconfigured with a ten degree elevation and declination respectively.Further, as described with reference to FIG. 42, the sub-arrays arerigidly mounted with the upper band antenna assembly. The HB-IBR shownin FIG. 43 differs from the HB-IBR of FIG. 4 in that the HB-IBR of FIG.43 includes an upper band antenna array 4105 instead of a dish antenna4005A. The operation of cable assembly 4006, 4006A and 4006B is similarfor both embodiments. The control line 4008 operates as described abovewith reference to FIG. 41.

FIG. 44 illustrates an upper band antenna array 4105 in accordance withsome embodiments. The antenna array 410 includes a sub-array panel 4401having 16 cross-polarized patch antenna elements 4402. The beam width ofa typical single patch antenna element 4402 is roughly 60 to 70 degreesin elevation and in azimuth. When such antenna elements are arranged ina 4×4 matrix as with sub-array panel 4401, the gain of the compositeantenna elements may be estimated based upon the mathematical relationG=10×Log 10 (16), (or 12 dB), plus the gain of the antenna elementitself (about 9 dBi). As a result, the gain of sub-array panel 4401 isequal to the gain of the individual patch antenna plus the gain of thearray, resulting in sub-array panel having an estimated gain of 21 dBi.

The antenna array 4105 also includes a sub-array panel 4403. In FIG. 44,the sub-array panel 4403 is a composite sub-array, having a matrix of4×4 sub-array panels, such that a 16 element array of sub-arrays areconfigured. Such a composite array 4403 results in a matrix of 16×16patch antenna elements. The antenna beam width of such a compositesub-array 4403 is roughly ¼ of the beam width of sub-array 4401 due tothe effective aperture of the antenna being four times as large. Thegain also increases by 10*Log 10 of 16 (or 12 dB), resulting in anoverall gain of 33 dBi (9+12+12) and an estimated beam width ofapproximately 3 degrees.

In FIG. 44, the upper band array 4105 includes a matrix of 64×64 antennapatches, each of which is a matrix of 4×4 composite sub-array panels(e.g., sub-array panel 4403). This results in a 4096 antenna elementarray with cross-polarization per element. The gain of upper band array4105 is equal to approximately the gain of an individual patch element 9dBi plus the upper and array gain of 12 dB+composite sub-array 12dB+sub-array 12 dB, resulting in a total array gain of approximately 45dBi.

In FIG. 44, the spacing of the individual patch antenna elements is 0.75wavelengths in a square matrix. It will be appreciated that alternativespacing and geometries are contemplated, such as a so-called hexagonalspacing, and spare array spacing approaches, and alternative wavelengthsare also contemplated.

Referring now to FIG. 45, additional details associated with antennaarray 4105 are described, including exemplary embodiments of theprocessing, control, and distribution of signals for each antennaelement, sub-array, and composite sub-array. Antenna sub-array panel4401 is shown in relation to electronics 4501A. The electronics 4501Ainclude two amplifiers and two phase shifters (only a single set isshown in FIG. 45). It will be appreciated that a pair of variable gainamplifier 4503A and a pair of variable phase shifter 4502A arecontrolled by four control lines. Such control is applied to twocross-pole RF signals entering electronics 4501A to be utilized for theorthogonal polarizations (cross-pol) capability of the antenna element4402, for example. Alternative embodiments may include switches for thedistribution of the RF signals to one or the other polarization of theantenna element, or only provide for a single linear, or circularlypolarized antenna capability.

In the embodiment of FIG. 45, the two cross-pole signals each have avariable gain 4503A and a variable phase 4502A applied to themindependently. Each of the two cross-pole signals are then distributedcommonly to each of the 16 elements of sub-array 4401. As a result, all16 vertical polarized (V-Pol) transmissions and all horizontal (H-Pol)transmissions receive the same gain and phase adjustment. This does not,of course, limit differences in the gains or phases from each elementdue to fixed offsets designed into the array, nor does it limit the useof alternative polarization approaches. As discussed, the variable gainand variable phase shift, having been applied to one of the cross-polesignals, is distributed to one of the polarizations of each of the patchantennas of the matrix of 16×16 patch antennas associated with sub-arraypanel 4401, each having a common polarization. This may be accomplishedusing, for example, a Wilkinson divider, or other techniques known inthe art.

The other variable gain and variable phase shifter (also of 4403A and4402A) is then applied to the other cross-polarization signal anddistributed to the other cross-polarizations of the same patch antennaswith a respective opposite common polarization. The electronics 4501A ofsub-array panel 4401 are arranged in a 16×16 matrix which is configuredas described above with respect to composite sub-array 4403 of FIG. 44.The sub-array panel 4403 includes sub-arrays 4501A through 4501P, withfour sub-array panels by four sub-array panels resulting in 16 sub-arraypanels. The electronics 4510A includes a dual splitter 4511A (one foreach cross-polarization signal) which distributes RF signals for bothpolarizations to each sub-array panel and associated electronics 4501Athrough 4501P. The control lines for electronics 4501A include two gainsand two phase control lines, a gain and a phase for the verticalpolarization and a gain and a phase for the horizontal polarization,each of which is common to all 16 elements of 4401. Each sub-array paneland electronics 4501A through 4501P has unique gain and phase controlsfor each of the vertical and horizontal polarizations, resulting in 16×4control lines entering composite sub-array 4510A and distributed to eachsub-array 4501A through 4501P.

Referring now to array 4105, the array 4105 includes compositesub-arrays 4520A through 4520P which include 16 sub-arrays 4501A. Theelectronics associated with the distribution of RF signals from CBR4002A utilizing cable assembly 4007 is distributed with splitter 4521which includes both vertical and horizontal polarizations eachdistributed to one composite sub-array panel 4520A through 4520P. IBR4003 a controls the steerable antenna array utilizing control lineassembly 4006, resulting in 128 control lines allowing control of groupsof 16 antenna elements and associated cross-polarized gains and phasesdistinctly allowing for sub-arrays 4501A through 4501P to be controlledin gain and phase for each polarization uniquely.

It will be appreciated that the arrangement may differ from that shownin FIG. 45, including, for example, the arrangement may includegroupings of more or less elements per sub-array, more or less overallnumbers of elements within the complete electronically controllablearray, and the like. Additionally, it will be appreciated that thecontrol lines of 4006 may carry voltage, current, messaging, digitallyencoded, etc., as known in the art. Further while RF signaling and RFdividers are shown for the cross-pole signals of 4007 and distributed tothe phase array or beam former weighting circuitry 4501A through 4501Pother embodiments may include digital signaling with transceiversdistributed on a sub-array basis or collectively for the entire antennaarray.

While not specifically discussed with reference to FIG. 45, one ofordinary skill in the art will recognize that similar arrangements tothose of the embodiments of FIG. 45 may be utilized for the receptionprocess instead of a phase array transmission process. For example,rather than the variable gain amplifiers 4503A being set to amplify theRF signals from the input from the composite sub-array 4510A, theamplifier may perform a variable gain amplification from the sub-array4501A to the composite sub-array 4510A. The operation of the variablephase shifters (cross-Pol) 4502A includes receiving a signal from thesummed patch antenna elements used for the reception of incomingsignals, imparting a specific phase shift to each of the cross polsignals, and providing the phase shifted signals to the variable gainamplifiers (4502A). In this example, the splitters of the array,composite sub-array, and composite sub array operate as summers.Additionally, as discussed elsewhere in the specification, atransmit/receive switch may be utilized to switch between the receiveand transmit time periods for time division operation. Alternatively, afrequency division duplexed configuration may be supported by utilizinga duplexer, as previously discussed to couple the receive antennaweighting elements and the transmitter antenna weighting elements to theantenna elements, rather than transmit and receive switch as discussed.

Exemplary embodiments of the HB-IBR and various elements of the HB-IBRhave been described with reference to FIGS. 37-45. Embodiments furtherhave been described and contemplate utilizing embodiments and variouselements of the IBR described associated with FIGS. 5-36. Theseexemplary element embodiments may be assembled together in manydifferent combinations and permutations. A very short description of buta few of the possible overall HB-IBR exemplary embodiments is summarizedbriefly below, utilizing IBRs for the lower band radio and either a CBRor IBR for the upper band.

A first exemplary embodiment of an HB-IBR includes the features outlinedin Table 8.

TABLE 8 First Exemplary Hybrid Band Intelligent Backhaul Radio FeaturesLower band IBR (e.g., IBR of Table 1) Upper Band IBR FDD OperationSC-FDE Modulation K = 1, M = 1 L = 1, N = 1 Q = 1 Upper Band Dish 40 dBiAntenna (e.g., Antenna of FIG. 42) 16 QAM ⅞ coding rate 1 stream fixedsuperframe (1 ms) NACK protocol up to 500 MHz channel bandwidth for eachthe receiver and transmitter single MPDU per PPDUEmbodiments of the exemplary HB-IBR configuration of Table 8 can providein excess of 3 GBPS aggregate HB-IBR throughput.

The lower band IBR configuration of Table 8 may utilize features of theIBR of Table 1. At 28 MHz symbol rate and channel bandwidth, 256 QAM, 2modulated streams, ⅞ rate coding, and with MAC and PHY efficiencies of95% and 90% respectively, the aggregate bi-directional throughput forthe lower band exemplary IBR embodiment can exceed 330 Mb/s with anaverage end to end latency of about 2 ms for this link individually.With respect to the upper band radio, 500 MHz modulation bandwidth isutilized for both the receive and transmitter in a frequency divisionduplexed configuration.

The upper band IBR (or CBR with equivalent single stream, single antennaconfiguration) provides a single direction bit rate of 500 MHz (symbolrate) (4 bits/Hz) (⅞ coding) equaling 1750 MBPS. The upper band radiocan have a very high MAC efficiency (ratio of MPDU payload bits tooverall MAC bits) under heavy loading from the IBR RLC—in excess of 95%,resulting in excess 1575 MBPS. The PHY efficiency for the upper bandradio generally exceeds 90% due to the generally line of sightoperation, resulting in a single direction throughput exceeding 1417MBPS. As a result, the throughput of the aggregate HB-IBR of Table 8 canexceed 3 GBPS when the low band throughput (330 MBPS) and each link ofthe FDD high band radio (2×1417 or 2835 MBPS) is used.

A second exemplary embodiment of an HB-IBR includes the featuresoutlined in Table 9.

TABLE 9 First Exemplary Hybrid Band Intelligent Backhaul Radio FeaturesLower band IBR (e.g., IBR of Table 1) Upper Band IBR TDD OperationSC-FDE Modulation K = 2, M = 2 L = 2, N = 2 Q = 2 (e.g., cross pol arrayof FIG. 43) Upper Band array 40 dBi Antenna (e.g., Antenna of FIG.43-FIG. 45) 16 QAM ⅞ coding rate 2 streams fixed superframe (1 ms) NACKprotocol up to 275 MHz channel bandwidth single MPDU per PPDUEmbodiments of the exemplary HB-IBR configuration of Table 9 provides inexcess of 2 GBPS aggregate throughput.

In some embodiments, the lower band IBR configuration of Table 9utilizes features of the IBR of Table 1. At 28 MHz symbol rate andchannel bandwidth, 256 QAM, 2 modulated streams, ⅞ rate coding, and withMAC and PHY efficiencies of 95% and 90% respectively, the aggregatebi-directional throughput for the lower band IBR can exceed 330 Mb/swith an average end to end latency of about 2 ms for this linkindividually. With respect to the upper band radio, a single 275 MHzbandwidth is utilized for both receive and transmit in a time divisionduplexed configuration.

The upper band IBR (or CBR with equivalent dual stream and dualpolarized antenna array configuration) provides peak data rate for bothdirections in aggregate of 1975 MBPS, including dual data streams, oneutilizing each upper band array polarization. Such a rate is determinedby the product of 350 MHz (symbol rate) (4 bits/Hz) (⅞ coding)(2streams) equaling 1975 MBPS. This exemplary embodiment of the upper bandradio of the an HB-IBR can have a very high MAC efficiency (ratio ofMPDU payload bits to overall MAC bits) under heavy loading from the IBRRLC—in excess of 95%, resulting in excess 1876 MBPS. The PHY efficiencyfor the upper band radio generally exceeds 90% due to the generally lineof sight operation, resulting in an aggregate bi-directional throughputexceeding 1688 MBPS. As a result, the HB-IBR of Table 9 has an aggregatethroughput that can exceed 2 GBPS when the low band through put (330MBPS) and the single link of the TDD high band radio (1688 MBPS) isused.

One or more of the methodologies or functions described herein may beembodied in a computer-readable medium on which is stored one or moresets of instructions (e.g., software). The software may reside,completely or at least partially, within memory and/or within aprocessor during execution thereof. The software may further betransmitted or received over a network.

The term “computer-readable medium” should be taken to include a singlemedium or multiple media that store the one or more sets ofinstructions. The term “computer-readable medium” shall also be taken toinclude any medium that is capable of storing, encoding or carrying aset of instructions for execution by a machine and that cause a machineto perform any one or more of the methodologies of the presentinvention. The term “computer-readable medium” shall accordingly betaken to include, but not be limited to, solid-state memories, andoptical and magnetic media.

Embodiments of the invention have been described through functionalmodules at times, which are defined by executable instructions recordedon computer readable media which cause a computer, microprocessors orchipsets to perform method steps when executed. The modules have beensegregated by function for the sake of clarity. However, it should beunderstood that the modules need not correspond to discreet blocks ofcode and the described functions can be carried out by the execution ofvarious code portions stored on various media and executed at varioustimes.

It should be understood that processes and techniques described hereinare not inherently related to any particular apparatus and may beimplemented by any suitable combination of components. Further, varioustypes of general purpose devices may be used in accordance with theteachings described herein. It may also prove advantageous to constructspecialized apparatus to perform the method steps described herein. Theinvention has been described in relation to particular examples, whichare intended in all respects to be illustrative rather than restrictive.Those skilled in the art will appreciate that many differentcombinations of hardware, software, and firmware will be suitable forpracticing the present invention. Various aspects and/or components ofthe described embodiments may be used singly or in any combination. Itis intended that the specification and examples be considered asexemplary only, with a true scope and spirit of the invention beingindicated by the claims.

1-20. (canceled)
 21. An intelligent backhaul radio comprising: a firsttransmitter, wherein the first transmitter is configured to operate on afirst frequency channel utilizing first radio parameters as a firstcommunications link; a first receiver, wherein the first receiver isconfigured to operate on a second frequency channel utilizing secondradio parameters as a second communications link; and a controller incommunication with the first transmitter and the first receiver, thecontroller to control functions associated with the first and secondradio parameters and the first and second communication links, whereinone or more performance metrics of the first communications link areenhanced utilizing said second communications link; wherein said firsttransmitter comprises one or more fixed directional antennas fortransmission, and further comprises: one or more modulator cores,wherein each modulator core modulates a respective transmit datainterface stream to produce one or more transmit symbol streams; aplurality of transmit RF chains to convert from a plurality of transmitchain input signals to a plurality of respective transmit RF signals;and wherein said first receiver comprises an adaptive antenna array forreception and further comprises: one or more demodulator cores, whereineach demodulator core demodulates one or more receive symbol streams toproduce a respective receive data interface stream, a plurality ofreceive radio frequency (RF) chains to convert from a plurality ofreceive RF signals to a plurality of respective receive chain outputsignals; and a frequency selective receive path channel multiplexercoupled to the one or more demodulator cores and to the plurality ofreceive RF chains, the frequency selective receive path channelmultiplexer to produce the one or more receive symbol streams providedto the one or more demodulator cores from the plurality of receive chainoutput signals; wherein said adaptive antenna array comprises: aplurality of directive gain antenna elements; and a plurality of RFconnections to couple at least certain of the plurality of directivegain antenna elements to the plurality of receive RF chains.
 22. Theintelligent backhaul radio of claim 21, wherein a number of directivegain antenna elements that can be selectively coupled to receive RFchains exceeds a number of receive RF chains that can accept receive RFsignals from the plurality of RF connections.
 23. The intelligentbackhaul radio of claim 21, wherein said second frequency channel isdifferent than said first frequency channel.
 24. The intelligentbackhaul radio of claim 21, wherein said second frequency channeloccupies a different frequency band than a frequency band occupied bysaid first frequency channel.
 25. The intelligent backhaul radio ofclaim 21, wherein said second frequency channel and first frequencychannel occupy one or more of a lower and an upper band.
 26. Theintelligent backhaul radio of claim 21 wherein the enhancement of theone or more performance metrics of the first communications linkutilizing said second communications link results in an adaptation of amodulation and coding scheme (MCS).
 27. The intelligent backhaul radioof claim 26 wherein the modulation and coding scheme (MCS) is signaledutilizing the second communications link.
 28. The intelligent backhaulradio of claim 21 further comprising a transmit path channel multiplexercoupled to the one or more modulator cores and to the plurality oftransmit RF chains, the transmit path channel multiplexer to produce theplurality of transmit chain input signals provided to the plurality oftransmit RF chains from the one or more transmit symbol streams.
 29. Theintelligent backhaul radio of claim 21 wherein said first radioparameters comprise transmitter beam forming weights.
 30. Theintelligent backhaul radio of claim 29 wherein the enhancement of theone or more performance metrics of the first communications linkutilizing said second communications link comprises adjustment of saidfirst radio parameters.
 31. The intelligent backhaul radio of claim 21wherein the enhancement of the one or more performance metrics of thefirst communications link utilizing said second communications linkcomprises adjustment of said first radio parameters.
 32. The intelligentbackhaul radio of claim 31 wherein said first radio parameters comprisesone or more of a transmit power control setting, a modulation and codingcontrol value, and transmitter polarization setting, a transmitterequalization setting, and a transmit beam former setting.
 33. Theintelligent backhaul radio of claim 21 wherein the enhancement of theone or more performance metrics of the first communications linkutilizing said second communications link comprises communication ofradio link controller (RLC) control frames from a second intelligentbackhaul radio in communication with the intelligent backhaul radio toan RLC in the intelligent backhaul radio resulting in a change to themodulation and coding scheme (MCS) and transmit power control values forthe first transmitter on a relative basis.
 34. The intelligent backhaulradio of claim 21 wherein the enhancement of the one or more performancemetrics of the first communications link utilizing said secondcommunications link comprises communication of RLC control frames from asecond intelligent backhaul radio in communication with the intelligentbackhaul radio to an RLC in the intelligent backhaul radio resulting ina change to the modulation and coding scheme (MCS) and transmit powercontrol values for the first transmitter on an absolute basis.
 35. Asystem comprising: a first intelligent backhaul radio comprising: afirst transmitter, wherein the first transmitter is configured tooperate on a first frequency channel utilizing first radio parameters asa first communications link; a first receiver, wherein the firstreceiver is configured to operate on a second frequency channelutilizing second radio parameters as a second communications link; and afirst controller in communication with the first transmitter and thefirst receiver, the first controller to control functions associatedwith the first and second radio parameters and the first and secondcommunication links, wherein one or more performance metrics of thefirst communications link are enhanced utilizing said secondcommunications link; and wherein said first transmitter comprises one ormore first fixed directional antennas for transmission, and furthercomprises: one or more first modulator cores, wherein each firstmodulator core modulates a respective first transmit data interfacestream to produce one or more first transmit symbol streams; a pluralityof first transmit radio frequency (RF) chains to convert from aplurality of first transmit chain input signals to a plurality ofrespective first transmit RF signals; and wherein said first receivercomprises a first adaptive antenna array for reception and furthercomprises: one or more first demodulator cores, wherein each firstdemodulator core demodulates one or more second receive symbol streamsto produce a respective second receive data interface stream, aplurality of first receive radio frequency (RF) chains to convert from aplurality of second receive RF signals to a plurality of respectivesecond receive chain output signals; a first frequency selective receivepath channel multiplexer coupled to the one or more first demodulatorcores and to the plurality of first receive RF chains, the firstfrequency selective receive path channel multiplexer to produce the oneor more second receive symbol streams provided to the one or more firstdemodulator cores from the plurality of second receive chain outputsignals; wherein said first adaptive antenna array comprises: aplurality of first directive gain antenna elements; a plurality of firstRF connections to couple at least certain of the plurality of firstdirective gain antenna elements to the plurality of first receive RFchains, and a second intelligent backhaul radio comprising: a secondtransmitter, wherein the second transmitter is configured to operate onthe second frequency channel utilizing third radio parameters as thesecond communications link; a second receiver, wherein the secondreceiver is configured to operate on the first frequency channelutilizing fourth radio parameters as the first communications link; anda second controller in communication with the second transmitter and thesecond receiver, the second controller to control functions associatedwith the third and fourth radio parameters and the first and secondcommunication links, wherein one or more performance metrics of thesecond communications link are enhanced utilizing said firstcommunications link; wherein said second transmitter comprises one ormore second fixed directional antennas for transmission, and furthercomprises: one or more second modulator cores, wherein each secondmodulator core modulates a respective second transmit data interfacestream to produce one or more second transmit symbol streams; aplurality of second transmit RF chains to convert from a plurality ofsecond transmit chain input signals to a plurality of respective secondtransmit RF signals; and wherein said second receiver comprises a secondadaptive antenna array for reception and further comprises: one or moresecond demodulator cores, wherein each second demodulator coredemodulates one or more first receive symbol streams to produce arespective first receive data interface stream, a plurality of secondreceive radio frequency (RF) chains to convert from a plurality of firstreceive RF signals to a plurality of respective first receive chainoutput signals; a second frequency selective receive path channelmultiplexer coupled to the one or more second demodulator cores and tothe plurality of second receive RF chains, the second frequencyselective receive path channel multiplexer to produce the one or morefirst receive symbol streams provided to the one or more seconddemodulator cores from the plurality of first receive chain outputsignals; wherein said second adaptive antenna array comprises: aplurality of second directive gain antenna elements; and a plurality ofsecond RF connections to couple at least certain of the plurality ofsecond directive gain antenna elements to the plurality of secondreceive RF chains.
 36. The system of claim 35, wherein the number offirst or second directive gain antenna elements of the respective firstor second intelligent backhaul radio that can be selectively coupled tofirst or second receive RF chains exceeds the number of respective firstor second receive RF chains that can accept respective first or secondreceive RF signals from the respective plurality of first or second RFconnections.
 37. The system of claim 35, wherein said second frequencychannel is different than said first frequency channel.
 38. The systemof claim 35, wherein said second frequency channel occupies a differentfrequency band than a frequency band occupied by said first frequencychannel.
 39. The system of claim 35, wherein said second frequencychannel and first frequency channel occupy one or more of a lower and anupper band.
 40. The system of claim 35 wherein the enhancement of theone or more performance metrics of the first communications linkutilizing said second communications link results in an adaptation of amodulation and coding scheme (MCS).
 41. The system of claim 40 whereinthe modulation and coding scheme (MCS) is signaled utilizing the secondcommunications link.
 42. The system of claim 35 wherein said firstintelligent backhaul radio further comprises a first transmit pathchannel multiplexer coupled to the one or more first modulator cores andto the plurality of first transmit RF chains, the first transmit pathchannel multiplexer to produce the plurality of first transmit chaininput signals provided to the plurality of first transmit RF chains fromthe one or more first transmit symbol streams.
 43. The system of claim35 wherein said first radio parameters comprise transmit beam formerweights.
 44. The system of claim 35 wherein the enhancement of the oneor more performance metrics of the first communications link utilizingsaid second communications link comprises adjustment of said first radioparameters.
 45. The system of claim 35 wherein the enhancement of theone or more performance metrics of the first communications linkutilizing said second communications link results in setting atransmitter power control level at the first transmitter.
 46. The systemof claim 35 wherein the enhancement of the one or more performancemetrics of the first communications link utilizing said secondcommunications link involves the communication of radio link controller(RLC) control frames from a second RLC within said second intelligentbackhaul radio to a first RLC in said first intelligent backhaul radioresulting in a change to the modulation and coding scheme and thetransmit power control values for the first transmitter on either arelative or absolute basis.
 47. The system of claim 35 wherein theenhancement of the one or more performance metrics of the firstcommunications link utilizing said second communications link comprisesadjustment of said first radio parameters.
 48. The system of claim 47wherein said first radio parameters comprises one or more of a transmitpower control setting, a modulation and coding control value, andtransmitter polarization setting, a transmitter equalization setting,and a transmitter beam former setting.